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AJCPP 2023
Program
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A-1
Combustion (1)
Combustion (1)
Details
Date
March Thu 16, 2023 08:40 - 10:20
Room
Room A
Chairperson
1
Analysis of wall temperature of ceramic matrix composites combustor
1
Analysis of wall temperature of ceramic matrix composites combustor
Speaker
Lu Zhang(Nanjing University of Aeronautics and Astronautics)
169
Characteristics of the OH Radical Chemiluminescence in Kerosene Lifted-flame According to the Position of Ultrasonic Standing Wave
169
Characteristics of the OH Radical Chemiluminescence in Kerosene Lifted-flame According to the Position of Ultrasonic Standing Wave
Speaker
ChangHan Bae(Pukyong National University)
13
2-D CFD analysis of mixing and turbulent combustion phenomena in coaxial rocket injectors
13
2-D CFD analysis of mixing and turbulent combustion phenomena in coaxial rocket injectors
Speaker
MIYOSHI Taisei(Kanazawa Institute of Technology)
107
Development of an artificial neural network for NH3/H2 combustion simulation with an improved chemical mechanism
107
Development of an artificial neural network for NH3/H2 combustion simulation with an improved chemical mechanism
Speaker
Serang Kwon(Korea University)
153
Mesoscale Surface Combustion Modeling of Metalized Solid Fuel
153
Mesoscale Surface Combustion Modeling of Metalized Solid Fuel
Speaker
HongSuk Choi(Seoul National University)
A-2
Combustion (2)
Combustion (2)
Details
Date
March Thu 16, 2023 10:40 - 12:00
Room
Room A
Chairperson
130
Large eddy simulation of dynamic analysis of methane / air non-premixed combustion in dual-swirl combustor
130
Large eddy simulation of dynamic analysis of methane / air non-premixed combustion in dual-swirl combustor
Speaker
Yuanhong Qi(Institute of Engineering Thermophysics, CAS，University of Chinese Academy of Sciences)
138
Effect of different injector arrangement on combustion characteristics of ATR engine LOX/kerosene rich gas generator
138
Effect of different injector arrangement on combustion characteristics of ATR engine LOX/kerosene rich gas generator
Speaker
yuankun zhang( Institute of Engineering Thermophysics, CAS，School of Aeronautics and Astronautics,UCAS)
109
Reactive-flow numerical simulation of an aero engine combustor with Immersed boundary method
109
Reactive-flow numerical simulation of an aero engine combustor with Immersed boundary method
Speaker
Taisuke Nambu(Japan Aerospace Exploration Agency)
110
Cold-flow numerical simulation of an aero engine combustor with Immersed boundary method.
110
Cold-flow numerical simulation of an aero engine combustor with Immersed boundary method.
Speaker
Tani Naoki(IHI Corporation)
A-3
OS3: Detonation and Pulsed Combustion (1)
OS3: Detonation and Pulsed Combustion (1)
Details
Date
March Thu 16, 2023 14:20 - 16:00
Room
Room A
Chairperson
84
Operating Condition of a Miniature Gas Turbine with a Pulse Combustor
84
Operating Condition of a Miniature Gas Turbine with a Pulse Combustor
Speaker
Sora Inoue(Graduate School of Systems Design, Tokyo Metropolitan University)
86
Experimental Study on Thrust Performance of Cylindrical Rotating Detonation Rocket Engine with Liquid Ethanol – Liquid Nitrous Oxide
86
Experimental Study on Thrust Performance of Cylindrical Rotating Detonation Rocket Engine with Liquid Ethanol – Liquid Nitrous Oxide
Speaker
Kazuki Ishihara(Nagoya University)
99
Fuel concentration measurement in a methane-oxygen rotating detonation engine
99
Fuel concentration measurement in a methane-oxygen rotating detonation engine
Speaker
NGHIA DUONG(Yokohama National University)
187
Experimental Study of Detonation Cell Size in Nitrous Oxide Hydrogen/Methane/Acetylene
187
Experimental Study of Detonation Cell Size in Nitrous Oxide Hydrogen/Methane/Acetylene
Speaker
BORAM JEON(Korea Aerospace University)
55
Characteristics of laser-induced sparks as an ignition source under various density conditions
55
Characteristics of laser-induced sparks as an ignition source under various density conditions
Speaker
Jieun Kang(Korea university，Department of Mechanical Engineering)
A-4
Jet Engine and Others
Jet Engine and Others
Details
Date
March Thu 16, 2023 16:20 - 18:00
Room
Room A
Chairperson
163
Stacking Curve Optimization for the 2nd Rotor Blade of a Counter-Rotating Compressor with Genetic Algorithm
163
Stacking Curve Optimization for the 2nd Rotor Blade of a Counter-Rotating Compressor with Genetic Algorithm
Speaker
Yimeng Wang( Institute of Engineering Thermophysics, CAS，School of Aeronautics and Astronautics, UCAS)
214
Effect of Non-Axisymmetric Endwall Profile on Turbine Cascade Flow Field and Loss
214
Effect of Non-Axisymmetric Endwall Profile on Turbine Cascade Flow Field and Loss
Speaker
Chuxuan Wang(Northwestern Polytechnical University)
70
Research on Adjustment Strategies of Inlet Guide Vanes in Axial Flow Compressor in Compressed Air Energy Storage System
70
Research on Adjustment Strategies of Inlet Guide Vanes in Axial Flow Compressor in Compressed Air Energy Storage System
Speaker
Pengfei LI( Institute of Engineering Thermophysics，University of Chinese Academy of Sciences)
189
Simulink Based Two-Spool Mixed-Flow Turbofan Engine Performance Analysis Modeling Validation
189
Simulink Based Two-Spool Mixed-Flow Turbofan Engine Performance Analysis Modeling Validation
Speaker
Seungheon Lee(Department of Aerospace Engineering, Inha University)
223
Prediction of thermodynamic properties of hydrocarbon fuels with high compressibility factor considering singularity problems
223
Prediction of thermodynamic properties of hydrocarbon fuels with high compressibility factor considering singularity problems
Speaker
Jaeseung Kim(Department of Aerospace Engineering，Seoul National University)
A-5
OS3: Detonation and Pulsed Combustion (2)
OS3: Detonation and Pulsed Combustion (2)
Details
Date
March Fri 17, 2023 08:40 - 10:20
Room
Room A
Chairperson
239
Development progress report of detonation-based combustion mode switchable engine for fully-reusable suborbital spaceplane
239
Development progress report of detonation-based combustion mode switchable engine for fully-reusable suborbital spaceplane
Speaker
Shuji Ogawa(PD AeroSpace, LTD.)
198
Experiments on hydrogen-air pulse detonation combustor with air-cooling for more than 1 minute operation
198
Experiments on hydrogen-air pulse detonation combustor with air-cooling for more than 1 minute operation
Speaker
Haruto Tanaka(Graduate School of Science and Engineering, Saitama University)
170
Numerical and experimental study of actuation characteristics on H2/Air non-premixed rotating detonation engine
170
Numerical and experimental study of actuation characteristics on H2/Air non-premixed rotating detonation engine
Speaker
Faming Wang(Tokai University)
52
Wave Steepening Instability Caused by Hypergolic Detonation of High Test Peroxide-based Hypergol
52
Wave Steepening Instability Caused by Hypergolic Detonation of High Test Peroxide-based Hypergol
Speaker
Jeong Junyeong(Korea Advanced Institute of Science and Technology)
15
Modeling of Energy Discharge and Bridgewire Burst in Exploding Bridgewire Detonator System
15
Modeling of Energy Discharge and Bridgewire Burst in Exploding Bridgewire Detonator System
Speaker
Kyoungjin Kim(Kumoh National Institute of Technology)
A-6
OS3: Detonation and Pulsed Combustion (3)
OS3: Detonation and Pulsed Combustion (3)
Details
Date
March Fri 17, 2023 10:40 - 12:00
Room
Room A
Chairperson
128
Optical observation on combustion Instability in Rotating Detonation engine
128
Optical observation on combustion Instability in Rotating Detonation engine
Speaker
Hideyuki Tanno(Japan Aerospace Exploration Agency)
144
Numerical Investigation on the Effect of Sidewall Curvature on Detonation Propagation in Rotating Detonation Engine
144
Numerical Investigation on the Effect of Sidewall Curvature on Detonation Propagation in Rotating Detonation Engine
Speaker
Moeno Miyashita(Keio University)
165
Injection rate measurements and machine-learning based predictions with single-hole diesel injector
165
Injection rate measurements and machine-learning based predictions with single-hole diesel injector
Speaker
Jiho Park(Departement of Aerospace Engineering, Sejong University)
168
Analysis on effects of intake water injection on NOx emission of a compression ignition piston engine
168
Analysis on effects of intake water injection on NOx emission of a compression ignition piston engine
Speaker
Hyunwoo Song(Yonsei University)
A-7
OS5: Machine Learning (1)
OS5: Machine Learning (1)
Details
Date
March Fri 17, 2023 13:00 - 14:20
Room
Room A
Chairperson
59
Research on the Surrogate Model for Deviation Angle and Total Pressure Loss Prediction of the Compressor Based on Machine Learning Methods
59
Research on the Surrogate Model for Deviation Angle and Total Pressure Loss Prediction of the Compressor Based on Machine Learning Methods
Speaker
BoWen Ma(Chongqing Jiaotong University.China)
104
Inverse Design and Sensitivity Analysis of Scramjet Intakes Using Deep Learning
104
Inverse Design and Sensitivity Analysis of Scramjet Intakes Using Deep Learning
Speaker
Chihiro Fujio(Kyushu University)
117
Influence of Differential Terms in the Governing Equation on the State Identification of the Combustion Field of a Rocket Combustor with a Single Coaxial Injector
117
Influence of Differential Terms in the Governing Equation on the State Identification of the Combustion Field of a Rocket Combustor with a Single Coaxial Injector
Speaker
Shoya Takeshi(Nihon university)
125
Study on Anomaly Detection of a Spacecraft Propulsion System using Machine Learning
125
Study on Anomaly Detection of a Spacecraft Propulsion System using Machine Learning
Speaker
Kazushi Adachi(The University of Tokyo)
A-8
OS5: Machine Learning (2)
OS5: Machine Learning (2)
Details
Date
March Fri 17, 2023 14:40 - 16:00
Room
Room A
Chairperson
157
Koopman mode decomposition of combustion instabilities in a hydrogen-fueled ram combustor using a convolutional neural network
157
Koopman mode decomposition of combustion instabilities in a hydrogen-fueled ram combustor using a convolutional neural network
Speaker
Koichi Omi(The University of Tokyo)
182
Community structure of high-frequency combustion instability in a model rocket engine combustor
182
Community structure of high-frequency combustion instability in a model rocket engine combustor
Speaker
Kazuki Kawano(Tokyo University of Science)
196
A linearization technique for parameter idetification of rocket engine simulation model
196
A linearization technique for parameter idetification of rocket engine simulation model
Speaker
Noriyasu Omata(JAXA)
200
Flow Anomaly Detection with Inverse System Identification by Using Multiple Pressure Dynamic Response of Propulsion System
200
Flow Anomaly Detection with Inverse System Identification by Using Multiple Pressure Dynamic Response of Propulsion System
Speaker
Kohji Tominaga(Japan Aerospace Exploration Agency)
B-1
Propellant and Others
Propellant and Others
Details
Date
March Thu 16, 2023 08:20 - 10:20
Room
Room B
Chairperson
32
Understanding the Hygrothermal Aging Effects on the Combustion Process of the MTV Igniter under Nitrogen Atmosphere
32
Understanding the Hygrothermal Aging Effects on the Combustion Process of the MTV Igniter under Nitrogen Atmosphere
Speaker
JUYOUNG OH(Seoul National University)
28
The experimental analysis of the combustion characteristics of the electrically controlled solid propellants with various metal composition
28
The experimental analysis of the combustion characteristics of the electrically controlled solid propellants with various metal composition
Speaker
Daehong Lim(Department of Aerospace Engineering, Seoul National University)
76
Fuel management on Propulsion System Test Complex for KSLV-II
76
Fuel management on Propulsion System Test Complex for KSLV-II
Speaker
JANGHWAN LEE(Korea Aerospace Reseach Institute)
96
Storage characteristics of low-toxic hypergolic propellant
96
Storage characteristics of low-toxic hypergolic propellant
Speaker
Kyounghwan Lee(Hanbat National University)
114
Comparison of alternative ionic monopropellants: HEHN and ADN-H2O2
114
Comparison of alternative ionic monopropellants: HEHN and ADN-H2O2
Speaker
JuWon Kim(Korea Advanced Institute of Science and Technology)
191
A Study on the Optimum Design of Multi Propellants in Interior Ballistics Using Genetic Algorithm Optimization.
191
A Study on the Optimum Design of Multi Propellants in Interior Ballistics Using Genetic Algorithm Optimization.
Speaker
JINSEOK YOO(INHA UNIVERSITY)
B-2
Turbopump and Others
Turbopump and Others
Details
Date
March Thu 16, 2023 10:40 - 12:20
Room
Room B
Chairperson
90
New Thermodynamic Parameter for Cryogenic Cavitation derived by Numerical Analysis using Simplified Thermodynamic Model
90
New Thermodynamic Parameter for Cryogenic Cavitation derived by Numerical Analysis using Simplified Thermodynamic Model
Speaker
Shuichi Ichiki(School of Engineering, Tohoku University，Institute of Fluid Science, Tohoku University)
154
Experimental study on the operating characteristics of Tesla pump designed for liquid
154
Experimental study on the operating characteristics of Tesla pump designed for liquid
Speaker
Hisana Sugimoto(Department of Advanced Energy，Graduate School of Frontier Science，the University of Tokyo)
120
Quantification of Blade-Cavity Interaction Under Two-Bladed Inducer Alternate Blade Cavitation
120
Quantification of Blade-Cavity Interaction Under Two-Bladed Inducer Alternate Blade Cavitation
Speaker
Youngkuk Yoon(Seoul National University)
126
Numerical Analysis of Rocket Pump Inducer with Backflow Restriction Step
126
Numerical Analysis of Rocket Pump Inducer with Backflow Restriction Step
Speaker
Takuo Mino(School of Engineering, Tohoku University，Institute of Fluid Science, Tohoku University)
156
Component tests of electric turbopump for rocket engines at low temperature environments.
156
Component tests of electric turbopump for rocket engines at low temperature environments.
Speaker
Shuichi TANABE(Chiba Institute of Technology)
B-3
Combustion and Others
Combustion and Others
Details
Date
March Thu 16, 2023 14:20 - 16:00
Room
Room B
Chairperson
245
Overview of Experimental and Numerical Researches on Plasma-assisted Ignition and Combustion in Scramjet/Aero-Engines
245
Overview of Experimental and Numerical Researches on Plasma-assisted Ignition and Combustion in Scramjet/Aero-Engines
Speaker
Shengyu Pang( Beijing Institute of Technology)
45
Spectroscopic Characteristics of Boron/1-butanol nanofuel droplet in Various Ambient Pressure Condition
45
Spectroscopic Characteristics of Boron/1-butanol nanofuel droplet in Various Ambient Pressure Condition
Speaker
Hyemin Kim(Korea National University of Transportation)
226
Estimation of Battery Mass for Upper Stage Launch Vehicle by Burning Time and Combustion Chamber Pressure
226
Estimation of Battery Mass for Upper Stage Launch Vehicle by Burning Time and Combustion Chamber Pressure
Speaker
Jungyeom Kim(Chungnam National University)
195
Effect of Injection Array on Combustion Dynamics in a Multi-element Model Combustor
195
Effect of Injection Array on Combustion Dynamics in a Multi-element Model Combustor
Speaker
Kibeom Lee(Kyungpook National University)
221
A Study on Injection Characteristics of Rectangular Injectors using Homogeneous Mixture and Eulerian to Lagrangian Transformation
221
A Study on Injection Characteristics of Rectangular Injectors using Homogeneous Mixture and Eulerian to Lagrangian Transformation
Speaker
Hoseok Chun(Department of Aerospace and Mechanical Engineering，School of Aerospace and Mechanical Engineering，Korea Aerospace University)
B-4
Liquid Rocket (1)
Liquid Rocket (1)
Details
Date
March Thu 16, 2023 16:20 - 18:00
Room
Room B
Chairperson
33
Experimental Study of Characteristics of Spray and Droplet in Liquid-Liquid Continuous Type Pintle Injector
33
Experimental Study of Characteristics of Spray and Droplet in Liquid-Liquid Continuous Type Pintle Injector
Speaker
Ingyu Lee(Seoul National University，Department of Aerospace Engineering)
53
A Multi-Ignitable and Deep Throttleable Methane Engine for Future In-Space Transport Systems
53
A Multi-Ignitable and Deep Throttleable Methane Engine for Future In-Space Transport Systems
Speaker
Byoungjik Lim(Small Launcher R&D Office，Korea Aerospace Research Institute)
93
Sloshing and Bubble Behavior Induced by Vertical Excitation
93
Sloshing and Bubble Behavior Induced by Vertical Excitation
Speaker
Kohjiro Mizumoto(School of Engineering，The University of Tokyo，Japan)
100
Real Gas Effects on Transcritical Reacting Flow Around a Cryogenic Methane/Oxygen Pintle Type Injector
100
Real Gas Effects on Transcritical Reacting Flow Around a Cryogenic Methane/Oxygen Pintle Type Injector
Speaker
Eliot Foss(University of Tokyo, Department of Aeronautics and Astronautics)
B-5
Hybrid Rocket (1)
Hybrid Rocket (1)
Details
Date
March Fri 17, 2023 09:20 - 10:20
Room
Room B
Chairperson
249
A performance comparison of electrically controlled solid propellants of selective metal additives
249
A performance comparison of electrically controlled solid propellants of selective metal additives
Speaker
Rajendra Rajak(Seoul National University, Republic of Korea)
178
Local Regression Rate of Vortex Flow Pancake Hybrid Rocket Motor with Different Injection Angles
178
Local Regression Rate of Vortex Flow Pancake Hybrid Rocket Motor with Different Injection Angles
Speaker
Lee JungYong(Korea Aerospace University，Graduate School of Smart Air Mobility)
85
Combustion test of SOFT Hybrid Rocket Engine with LOX Regenerative-cooling Nozzle
85
Combustion test of SOFT Hybrid Rocket Engine with LOX Regenerative-cooling Nozzle
Speaker
Naoki Yabe(Graduate School of Systems Design, Tokyo Metropolitan University)
B-6
Hybrid Rocket (2)
Hybrid Rocket (2)
Details
Date
March Fri 17, 2023 10:40 - 12:00
Room
Room B
Chairperson
27
Study on the Method of Measuring Real Time O/F of a Hybrid Rocket
27
Study on the Method of Measuring Real Time O/F of a Hybrid Rocket
Speaker
Ichiro Nakagawa(Tokai university)
177
A Study on the Local Regression Rate of Paraffin Slab-burner Using Photogrammetry Technique
177
A Study on the Local Regression Rate of Paraffin Slab-burner Using Photogrammetry Technique
Speaker
JooHyun Lee(Korea Aerospace University)
11
Basic investigation on the regression rate enhancement of the hybrid rocket by applying kerosene on the plastic fuel as combustion improver
11
Basic investigation on the regression rate enhancement of the hybrid rocket by applying kerosene on the plastic fuel as combustion improver
Speaker
Ohtoshi Mikio(Department of aeronautics, Kanazawa Institute of Technology)
9
Numerical analysis of novel auxiliary kerosene jet flow to enhance regression rate of the hybrid rocket with recycled plastic fuel
9
Numerical analysis of novel auxiliary kerosene jet flow to enhance regression rate of the hybrid rocket with recycled plastic fuel
Speaker
Mikio Ohtoshi(Department of aeronautics, Kanazawa Institute of Technology )
B-7
Space Propulsion (1)
Space Propulsion (1)
Details
Date
March Fri 17, 2023 13:00 - 14:20
Room
Room B
Chairperson
197
Conceptual System Analysis of Very-Low-Earth-Orbit Satellites with Atmosphere-Breathing Electric Propulsion
197
Conceptual System Analysis of Very-Low-Earth-Orbit Satellites with Atmosphere-Breathing Electric Propulsion
Speaker
Eunji Jun(Korea Advanced Institute of Science & Technology (KAIST))
204
Study on Hydrogen Catalytic Ignition for Application to Space Propulsion System
204
Study on Hydrogen Catalytic Ignition for Application to Space Propulsion System
Speaker
Minsig Hwang(Department of Aerospace Engineering，Inha University，Republic of Korea)
225
Satellite Plume Analysis Using Open Softwares
225
Satellite Plume Analysis Using Open Softwares
Speaker
SeungMin Lee(Gyeongsang National University)
230
Plume magnetic field and current density measurement of high-power AF-MPDT
230
Plume magnetic field and current density measurement of high-power AF-MPDT
Speaker
Yimeng Wang(Beihang university)
B-8
Space Propulsion (2)
Space Propulsion (2)
Details
Date
March Fri 17, 2023 14:40 - 16:00
Room
Room B
Chairperson
51
Sub-scale Demonstration of an Axial Magnetic Nozzle for Fusion Propulsion
51
Sub-scale Demonstration of an Axial Magnetic Nozzle for Fusion Propulsion
Speaker
Nathan Schilling(Kyushu University)
47
Electric-field simulation of a CubeSat FEEP thruster
47
Electric-field simulation of a CubeSat FEEP thruster
Speaker
Jeongsik Shin(Sejong University)
61
Thermoelectric Cooling Analysis of Gallium Propellant for Field Emission Electric Propulsion
61
Thermoelectric Cooling Analysis of Gallium Propellant for Field Emission Electric Propulsion
Speaker
Hyeonsu Jeong(Sejong University)
97
Design and verification of propulsion system simulator based on the cold gas thruster
97
Design and verification of propulsion system simulator based on the cold gas thruster
Speaker
Yehyun Kim(KAIST Satellite Technology Research Center)
C-1
OS4: Hypersonic Air-breathing Engine (1)
OS4: Hypersonic Air-breathing Engine (1)
Details
Date
March Thu 16, 2023 08:20 - 10:20
Room
Room C
Chairperson
203
A Study on the Conceptual Design of Two-Dimensional Variable Inlet
203
A Study on the Conceptual Design of Two-Dimensional Variable Inlet
Speaker
Youngjin Kim(Department of Aerospace Engineering, Inha University)
67
Thermal Evaluation of a Hypersonic Vehicle Airframe with TBCC Engine by Thermo-Fluid Coupled Analysis
67
Thermal Evaluation of a Hypersonic Vehicle Airframe with TBCC Engine by Thermo-Fluid Coupled Analysis
Speaker
Kotaro Yamada(Keio University)
162
Quasi-1D Analysis of a Supersonic Combutor According to the Injection Method of Liquid Hydro-carbon Fuel
162
Quasi-1D Analysis of a Supersonic Combutor According to the Injection Method of Liquid Hydro-carbon Fuel
Speaker
Sangwook Jin(KAIST，ADD)
41
Effects of film coolant combustion on regenerative cooling/film cooling performance for hydrocarbon fueled scramjet engine
41
Effects of film coolant combustion on regenerative cooling/film cooling performance for hydrocarbon fueled scramjet engine
Speaker
Jingying Zuo(Harbin Institute of Technology)
205
Development Status of the Air-turbo Rocket Engine “ATRIUM”
205
Development Status of the Air-turbo Rocket Engine “ATRIUM”
Speaker
Hiroaki Kobayashi(Waseda University)
209
Sub-scale Flight Test Plan for ATRIUM Engine Development
209
Sub-scale Flight Test Plan for ATRIUM Engine Development
Speaker
Yuki SAKAMOTO(Japan Aerospace Exploration Agency)
C-2
OS4: Hypersonic Air-breathing Engine (2)
OS4: Hypersonic Air-breathing Engine (2)
Details
Date
March Thu 16, 2023 10:40 - 12:20
Room
Room C
Chairperson
36
Experimental Study of Instability of Hydrocarbon Flow in a Regenerative Cooling Channel of Scramjet Engine
36
Experimental Study of Instability of Hydrocarbon Flow in a Regenerative Cooling Channel of Scramjet Engine
Speaker
Sato Hiroshi(Air Systems Research Center，Acquisition, Technology & Logistics Agency，Japan Ministry of Defense)
65
Suppression of scramjet unstart using boundary layer suction
65
Suppression of scramjet unstart using boundary layer suction
Speaker
Hwang Jeongjae(Korea University)
42
Development of a Scaled, Ground Test Model of a Turbine-Based Combined Cycle Engine
42
Development of a Scaled, Ground Test Model of a Turbine-Based Combined Cycle Engine
Speaker
Inyoung Yang(Korea Aerospace Research Institute)
17
Numerical simulation of orifice injection characteristics of hydrocarbon aviation fuel up to the critical temperature.
17
Numerical simulation of orifice injection characteristics of hydrocarbon aviation fuel up to the critical temperature.
Speaker
Sungrok Hwang(Pukyong National University)
250
Aerodynamic heating fluctuation in a hypersonic turbulent ramp flow
250
Aerodynamic heating fluctuation in a hypersonic turbulent ramp flow
Speaker
Zhenyuan Tang(Tsinghua University)
C-3
OS4: Hypersonic Air-breathing Engine (3)
OS4: Hypersonic Air-breathing Engine (3)
Details
Date
March Thu 16, 2023 14:20 - 16:00
Room
Room C
Chairperson
193
Design of a Turbine-Based Combined Cycle Engine Inlet for a Ground Test
193
Design of a Turbine-Based Combined Cycle Engine Inlet for a Ground Test
Speaker
Yangji Lee(Korea Aerospace Research Institute)
26
Quasi-one-dimensional code development for solving the mode transition and thermal choking in the scramjet combustor
26
Quasi-one-dimensional code development for solving the mode transition and thermal choking in the scramjet combustor
Speaker
Jaehyun Nam(Department of Aerospace Engineering, Seoul National University)
10
2D Numerical investigation on the turbulent flow of the scramjet flame holder
10
2D Numerical investigation on the turbulent flow of the scramjet flame holder
Speaker
Kotaro Iguchi(Kanazawa Institute of Technology)
105
Numerical Investigation on the Effects of the Exit Nozzle Throat Height on the Buzz Characteristics Occurring in the Hypersonic Intake for High Mach Integrated Control Experiment (HIMICO)
105
Numerical Investigation on the Effects of the Exit Nozzle Throat Height on the Buzz Characteristics Occurring in the Hypersonic Intake for High Mach Integrated Control Experiment (HIMICO)
Speaker
Manami Fujii(Waseda University)
133
Experimental Investigation on the Effects of the Bleed System on A Ramjet-Intake of High Mach Integrated Control Experiment (HIMICO)
133
Experimental Investigation on the Effects of the Bleed System on A Ramjet-Intake of High Mach Integrated Control Experiment (HIMICO)
Speaker
Yuki Fujimori(Waseda University)
C-4
OS4: Hypersonic Air-breathing Engine (4)
OS4: Hypersonic Air-breathing Engine (4)
Details
Date
March Thu 16, 2023 16:20 - 18:00
Room
Room C
Chairperson
148
Test Analysis of Isolator Design in a Dual-mode Ramjet with Kerosene Combustion
148
Test Analysis of Isolator Design in a Dual-mode Ramjet with Kerosene Combustion
Speaker
JAEHO LEE(Hyundai-Rotem)
155
Modal Analysis of Forced Ignition Characteristics by Micro-Rocket Torch in Supersonic Flow
155
Modal Analysis of Forced Ignition Characteristics by Micro-Rocket Torch in Supersonic Flow
Speaker
Shinichiro Ogawa(Osaka Metropolitan University)
192
Tomographic Reconstruction of Flowfields Around A Hypersonic Winged-Aircraft Model in Large-Scale Hypersonic Wind Tunnel Experiments
192
Tomographic Reconstruction of Flowfields Around A Hypersonic Winged-Aircraft Model in Large-Scale Hypersonic Wind Tunnel Experiments
Speaker
Hidemi Takahashi(Japan Aerospace Exploration Agency)
140
Vitiation Effects on Combustion Characteristics of a Supersonic Combustor Model for JAXA RD1 Flight Experiment at Mach 6 Flight Conditions
140
Vitiation Effects on Combustion Characteristics of a Supersonic Combustor Model for JAXA RD1 Flight Experiment at Mach 6 Flight Conditions
Speaker
Masahiro TAKAHASHI(JAXA Kakuda Space Center)
194
Subsonic combustion performance according to fuel injector configuration in a Dual-Mode Scramjet(DMS) Combustor
194
Subsonic combustion performance according to fuel injector configuration in a Dual-Mode Scramjet(DMS) Combustor
Speaker
Kyungjae LEE(Korea Aerospace Research Institute)
C-5
OS4: Hypersonic Air-breathing Engine (5)
OS4: Hypersonic Air-breathing Engine (5)
Details
Date
March Fri 17, 2023 08:40 - 10:20
Room
Room C
Chairperson
219
Performance Modeling of an Isolator for a Dual Mode Ramjet
219
Performance Modeling of an Isolator for a Dual Mode Ramjet
Speaker
Yun Donggyu(Korea Aerospace University，Department of Aerospace and Mechanical Eng)
72
Flow and Performance Characteristics of a Streamline-traced Air Inlet Designed at Mach 2 for the ATRIUM Engine
72
Flow and Performance Characteristics of a Streamline-traced Air Inlet Designed at Mach 2 for the ATRIUM Engine
Speaker
Yusuke Maru(Japan Aerospace Exploration Agency)
127
Design and numerical simulation of REST intakes for on- and off-design condition
127
Design and numerical simulation of REST intakes for on- and off-design condition
Speaker
Daegi Yeom(Korea university, mechanical engineering)
57
Two-line Technique Measurement of Water Vapor in Supersonic Reacted Flow Via TDLAS
57
Two-line Technique Measurement of Water Vapor in Supersonic Reacted Flow Via TDLAS
Speaker
Ito Ryota(Tohoku University)
171
Ignition study of scramjet combustor using a micro-pulse detonation engine (μPDE) as an ignitor
171
Ignition study of scramjet combustor using a micro-pulse detonation engine (μPDE) as an ignitor
Speaker
Min-Su Kim(Pusan National University)
C-6
Liquid Rocket (2)
Liquid Rocket (2)
Details
Date
March Fri 17, 2023 10:40 - 12:00
Room
Room C
Chairperson
208
Experimental and numerical study on atomization process of a Ethanol-LOX pintle injector.
208
Experimental and numerical study on atomization process of a Ethanol-LOX pintle injector.
Speaker
Takuto Wada(University of Tokyo)
190
Study of Small Liquid Rocket Supply System Composition and Dynamic M&S
190
Study of Small Liquid Rocket Supply System Composition and Dynamic M&S
Speaker
HyeIn Kim(Inha university, Aerospace Engineering)
167
Spray Angle Variation of Low-Temperature Gel Propellant Using Pressure Swirl Injector
167
Spray Angle Variation of Low-Temperature Gel Propellant Using Pressure Swirl Injector
Speaker
Donggeun Lee(Korea Aerospace University)
184
Large-Eddy Simulation of Recessed Shear Coaxial Injector at Supercritical Pressure
184
Large-Eddy Simulation of Recessed Shear Coaxial Injector at Supercritical Pressure
Speaker
TaeJun Jeon(Kyungpook National University)
C-7
Liquid Rocket (3)
Liquid Rocket (3)
Details
Date
March Fri 17, 2023 13:00 - 14:00
Room
Room C
Chairperson
141
Nonconformance control of KSLV-II, Nuri
141
Nonconformance control of KSLV-II, Nuri
Speaker
Sangyeon Cho(Korea Aerospace Research Institute)
151
Experiment study of instabilities for bipropellant thruster by throttling Hydrogen Peroxide
151
Experiment study of instabilities for bipropellant thruster by throttling Hydrogen Peroxide
Speaker
Vincent UGOLINI(KAIST(Korea Advanced Institute of Science and Technology))
19
Study on the hydrogen peroxide thruster with externally heated aerospike nozzle
19
Study on the hydrogen peroxide thruster with externally heated aerospike nozzle
Speaker
KOTARO MUNENAGA(Department of aeronautics, Kanazawa Institute of Technology )
C-8
Liquid Rocket (4)
Liquid Rocket (4)
Details
Date
March Fri 17, 2023 14:40 - 16:00
Room
Room C
Chairperson
5
Flow and Spray Characteristics of Metal Additive Manufactured Gas-Liquid Pintle Injectors for a Throttleable Rocket Engine
5
Flow and Spray Characteristics of Metal Additive Manufactured Gas-Liquid Pintle Injectors for a Throttleable Rocket Engine
Speaker
Subeom Heo(Seoul National University)
63
Combustion Characteristics of GOX/GCH4 Pintle Model Combustor
63
Combustion Characteristics of GOX/GCH4 Pintle Model Combustor
Speaker
DaeHwan Kim(Seoul National University)
103
Self-Pulsation Characteristics of Swirl Coaxial Injectors with Various Internal Geometric Parameters
103
Self-Pulsation Characteristics of Swirl Coaxial Injectors with Various Internal Geometric Parameters
Speaker
Hadong Jung(School of Mechanical Engineering, Chungbuk National University)
108
Introduction of flame cooling system for KSLV-II on the propulsion system test complex
108
Introduction of flame cooling system for KSLV-II on the propulsion system test complex
Speaker
Yoonho SONG(Korea Aerospace Research Institute(KARI))
D-1
OS7: Beamed Energy Propulsion (1)
OS7: Beamed Energy Propulsion (1)
Details
Date
March Thu 16, 2023 08:20 - 10:20
Room
Room D
Chairperson
24
Output Power Enhancement of UT-94 Gyrotron for Microwave Rocket Launch
24
Output Power Enhancement of UT-94 Gyrotron for Microwave Rocket Launch
Speaker
Manabe Ayuto(The University of Tokyo)
37
Fundamental experiment of laser plasma visualization for advanced space propulsion research
37
Fundamental experiment of laser plasma visualization for advanced space propulsion research
Speaker
Ryota Yasuda(Kanazawa Institute of Technology，The Japan society for aeronautical and space sciences)
68
Experimental Study on Plasma Decay for the Enhancement of Pulse Repetition Frequency in Microwave Rocket
68
Experimental Study on Plasma Decay for the Enhancement of Pulse Repetition Frequency in Microwave Rocket
Speaker
Kuniyoshi Tabata(Japan Aerospace Exploration Agency)
89
Hugoniot Analysis of Two-Dimensional Axisymmetric Laser Supported Detonation Wave Using Measured Propagation Velocity
89
Hugoniot Analysis of Two-Dimensional Axisymmetric Laser Supported Detonation Wave Using Measured Propagation Velocity
Speaker
Kenya Sugamura(The University of Tokyo)
94
Investigation of Flight Performance on Multi-parabola Thruster Propelled by Repetitive-pulses Laser and Examination of Tracking System
94
Investigation of Flight Performance on Multi-parabola Thruster Propelled by Repetitive-pulses Laser and Examination of Tracking System
Speaker
Yuya Hayadate(Department of Aerospace Engineering, Tohoku University)
112
Effect of chemical reaction in atmospheric millimeter-wave discharge under subcritical condition
112
Effect of chemical reaction in atmospheric millimeter-wave discharge under subcritical condition
Speaker
Soichiro Suzuki(Department of Aerospace Engineering, Tohoku University)
D-2
OS7: Beamed Energy Propulsion (2)
OS7: Beamed Energy Propulsion (2)
Details
Date
March Thu 16, 2023 10:40 - 12:20
Room
Room D
Chairperson
147
Numerical Investigation of Atomic Line Absorption Effect on Laser Sustained Argon Plasma
147
Numerical Investigation of Atomic Line Absorption Effect on Laser Sustained Argon Plasma
Speaker
Hiroshi Katsurayama(Tottori University)
175
Investigation of Generating Conditions of Fiber Laser-Sustained Plasma using various F-number
175
Investigation of Generating Conditions of Fiber Laser-Sustained Plasma using various F-number
Speaker
Seiichiro Takano(Shizuoka University)
113
Experimental Observation of Plasma Generation and Thrust Measurement for Microwave-driven In-tube Accelerator
113
Experimental Observation of Plasma Generation and Thrust Measurement for Microwave-driven In-tube Accelerator
Speaker
Yamada Toshiki(Tohoku University)
73
Material dependence of the propulsion performance by a very weak laser ablation
73
Material dependence of the propulsion performance by a very weak laser ablation
Speaker
Koichi Mori(Osaka Metropolitan University)
77
A study on energy balance of solar thermal system for solar thermal propulsion
77
A study on energy balance of solar thermal system for solar thermal propulsion
Speaker
Yasuhisa Oda(Setsunan University)
D-3
OS1: More Electric Aircraft (1)
OS1: More Electric Aircraft (1)
Details
Date
March Thu 16, 2023 14:20 - 16:00
Room
Room D
Chairperson
44
Effect of Aspect Ratio on Air-Cooling Performance in Interior Permanent Magnet (IPM) Motor Driving Aviation Fans at High Altitude
44
Effect of Aspect Ratio on Air-Cooling Performance in Interior Permanent Magnet (IPM) Motor Driving Aviation Fans at High Altitude
Speaker
Yu Ito(The University of Tokyo)
54
The Possibility of Hybrid Electric and All-electric Airplane using Battery or Fuel Cell
54
The Possibility of Hybrid Electric and All-electric Airplane using Battery or Fuel Cell
Speaker
Teruhisa YAMAKITA(New Industry Research Organization (NIRO))
224
Environmental test of lithium-ion batteries for electric pump systems
224
Environmental test of lithium-ion batteries for electric pump systems
Speaker
Minho Lee(Department of Aerospace Engeering, Chungnam National University)
115
System study of More Electric Engine (MEE) concept
115
System study of More Electric Engine (MEE) concept
Speaker
Kota Ohno(Aero Engine, Space & Defense Business Area, IHI Corporation)
152
Analysis and Proposal for Propulsion System of Electric Vertical Takeoff and Landing Aircraft
152
Analysis and Proposal for Propulsion System of Electric Vertical Takeoff and Landing Aircraft
Speaker
ZHONG LEI(Suwa University of Science)
D-4
OS1: More Electric Aircraft (2)
OS1: More Electric Aircraft (2)
Details
Date
March Thu 16, 2023 16:20 - 18:00
Room
Room D
Chairperson
185
Flight Test of ICE-Battery Hybrid Propulsion System for UAV
185
Flight Test of ICE-Battery Hybrid Propulsion System for UAV
Speaker
Poomin Park(Korea Aerospace Research Institute)
159
Challenges and Opportunities on the Application of Liquid Hydrogen-Cooled Superconducting Generators to Hydrogen-Fueled Electrified-Propulsion Aircraft
159
Challenges and Opportunities on the Application of Liquid Hydrogen-Cooled Superconducting Generators to Hydrogen-Fueled Electrified-Propulsion Aircraft
Speaker
Keiichi OKAI(Japan Aerospace Exploration Agency)
206
Design Study of SOFC/Gas Turbine Combined Cycle Propulsion
206
Design Study of SOFC/Gas Turbine Combined Cycle Propulsion
Speaker
Takayuki Kojima(Japan Aerospace Exploration Agency)
118
Power generation tests of single SOFC and flame holding tests of excess-fuel injector for a lab-scale SOFC/gas turbine hybrid system
118
Power generation tests of single SOFC and flame holding tests of excess-fuel injector for a lab-scale SOFC/gas turbine hybrid system
Speaker
Kyoji IMAMURA(Nihon university)
111
High-efficiency Thermal Control System for Electric Aircraft using Vapor-Liquid Two-phase Thermal Control Technology
111
High-efficiency Thermal Control System for Electric Aircraft using Vapor-Liquid Two-phase Thermal Control Technology
Speaker
Hiroki Nagai(Institute of Fluid Science, Tohoku University)
D-5
Measurement and Diagnostics
Measurement and Diagnostics
Details
Date
March Fri 17, 2023 08:40 - 10:20
Room
Room D
Chairperson
227
Application of Pressure-Sensitive Paint Measurement Technology in Pressure Measurement of Bowed Blade Surface
227
Application of Pressure-Sensitive Paint Measurement Technology in Pressure Measurement of Bowed Blade Surface
Speaker
XiangFu Lei(Northwestern Polytechnical University)
62
Introduction of Control System of Propulsion System Test Complex for Korea Space Launch Vehicle II
62
Introduction of Control System of Propulsion System Test Complex for Korea Space Launch Vehicle II
Speaker
Dongki Kim(Korea Aerospace Research Institute(KARI))
74
A Validation of Three-Dimensional Near-Wall Density Measurement with Background-Oriented Schlieren using Mirror
74
A Validation of Three-Dimensional Near-Wall Density Measurement with Background-Oriented Schlieren using Mirror
Speaker
Masahito Akamine(Graduate School of Engineering, the University of Tokyo)
158
Full Error Factor Analysis Method Based on TSP Calibration Experiment
158
Full Error Factor Analysis Method Based on TSP Calibration Experiment
Speaker
Bo Ouyang(Northwestern Polytechnical University)
215
A multimode six-degree-of-freedom thrust stand for micropropulsion and evaluation of its measurement performance
215
A multimode six-degree-of-freedom thrust stand for micropropulsion and evaluation of its measurement performance
Speaker
Isamu Moriai(The University of Tokyo)
D-6
Thruster and Others
Thruster and Others
Details
Date
March Fri 17, 2023 10:40 - 12:00
Room
Room D
Chairperson
121
An Experimental Ablation Study on Carbon Composite Materials
121
An Experimental Ablation Study on Carbon Composite Materials
Speaker
RAJESHKUMAR CHINNARAJ(Department of Aerospace Engineering,Jeonbuk National University)
149
numerical study of reacting flow for bi-propellant thruster
149
numerical study of reacting flow for bi-propellant thruster
Speaker
Hwanghui Jeong(NEXTFoam)
179
Design of Catalyst for Nitrous Oxide Catalytic Decomposition Monopropellant Thruster
179
Design of Catalyst for Nitrous Oxide Catalytic Decomposition Monopropellant Thruster
Speaker
Seungho Lee(Korea Advanced Institute of Science and Technology (KAIST))
246
One Dimensional Numerical Analysis of Laser Supported Detonation Driven by Near-Infrared Laser
246
One Dimensional Numerical Analysis of Laser Supported Detonation Driven by Near-Infrared Laser
Speaker
Kento Suzuki(Tottori University, Japan)
D-7
Air Breathing Engine
Air Breathing Engine
Details
Date
March Fri 17, 2023 13:00 - 14:20
Room
Room D
Chairperson
8
Study on Variable Ejector Rocket Engines with Ultra-high Bypass Ratio
8
Study on Variable Ejector Rocket Engines with Ultra-high Bypass Ratio
Speaker
Kenji Kobayashi(Sojo university)
16
Numerical analysis of over-expanded three-dimensional separated flow field in SERN
16
Numerical analysis of over-expanded three-dimensional separated flow field in SERN
Speaker
Yuepeng Mao(Chongqing Jiaotong University)
172
Numerical Investigation of Detailed Combustion Dynamics of a Hydrogen-fueled Scramjet Combustor depending on Fueling Schemes using High-resolution IDDES Simulation
172
Numerical Investigation of Detailed Combustion Dynamics of a Hydrogen-fueled Scramjet Combustor depending on Fueling Schemes using High-resolution IDDES Simulation
Speaker
SeungMin Jeong(Pusan National University)
150
Performance and Thermo-Fluid Analysis of Micro Turbojet Integrated Model at various Operating Conditions
150
Performance and Thermo-Fluid Analysis of Micro Turbojet Integrated Model at various Operating Conditions
Speaker
DongEun Lee(Department of Aerospace System Engineering，Aerospace Propulsion Research Division)
D-8
Acoustics
Acoustics
Details
Date
March Fri 17, 2023 14:40 - 16:00
Room
Room D
Chairperson
58
Noise Suppression Method for Rectangular Hypersonic Nozzle
58
Noise Suppression Method for Rectangular Hypersonic Nozzle
Speaker
Mori Toshiya(Graduate School of Science and Technology, Gunma University)
129
Noise reduction mechanism of an airfoil with spanwise-varying trailing-edge serrations
129
Noise reduction mechanism of an airfoil with spanwise-varying trailing-edge serrations
Speaker
Lei Wang(xi)
220
Proposing the Fan Noise Simulator as a new experimental method to assess acoustic characteristics of liners under grazing condition
220
Proposing the Fan Noise Simulator as a new experimental method to assess acoustic characteristics of liners under grazing condition
Speaker
Koki Tanaka(The University of Tokyo Department of Mechanical Engineering)
12
Investigation of the hypersonic jet noise reduction by the outer subsonic flow
12
Investigation of the hypersonic jet noise reduction by the outer subsonic flow
Speaker
Harada Masanor(Department of aeronautics, Kanazawa Institute of Technology)
E-1
OS6: Electric Propulsion (1)
OS6: Electric Propulsion (1)
Details
Date
March Thu 16, 2023 08:20 - 10:20
Room
Room E
Chairperson
160
Preliminary Experiment of High-Voltage Hall-thrusters
160
Preliminary Experiment of High-Voltage Hall-thrusters
Speaker
Ikkoh Funaki(JAXA)
234
Lifetime prediction of an orificed hollow cathode used for electric propulsion
234
Lifetime prediction of an orificed hollow cathode used for electric propulsion
Speaker
Shuai Cao(Shenzhen Campus of Sun Yat-sen University，Sun Yat-sen University)
217
Electron Emission Characteristics of LaB6 Electron Gun for Miniature Hall Thrusters
217
Electron Emission Characteristics of LaB6 Electron Gun for Miniature Hall Thrusters
Speaker
Aoma Fujimori(The University of Tokyo)
201
Emitter Temperature and plasma distribution inner LaB6 hollow cathode
201
Emitter Temperature and plasma distribution inner LaB6 hollow cathode
Speaker
Yuya Oshio(Ryukoku University)
229
5 kW Class Hall Thruster System Development for GEO satellite
229
5 kW Class Hall Thruster System Development for GEO satellite
Speaker
Holak Kim(Korea Aerospace Research Institute)
235
Evaluating the Performance of the 100 Kilo-watt Class Hall Thruster
235
Evaluating the Performance of the 100 Kilo-watt Class Hall Thruster
Speaker
Ning Guo(Lanzhou Institute of Physics)
E-2
OS6: Electric Propulsion (2)
OS6: Electric Propulsion (2)
Details
Date
March Thu 16, 2023 10:40 - 12:20
Room
Room E
Chairperson
188
Improvement of Miniature Hall thrusters
188
Improvement of Miniature Hall thrusters
Speaker
Shitara Satoru(Tokai University)
186
Improvement of Miniature Anode Layer Hall Thrusters
186
Improvement of Miniature Anode Layer Hall Thrusters
Speaker
Shigeru Sato(Tokai university)
123
Experiment and Modeling of Ion extraction of Porous Ionic Electrospray Thruster
123
Experiment and Modeling of Ion extraction of Porous Ionic Electrospray Thruster
Speaker
Takagi Koki(The University of Tokyo)
238
Performance of ARCH miniature ion thruster with double anode
238
Performance of ARCH miniature ion thruster with double anode
Speaker
Kunlong Wu(School of Space and Environment, Beihang University, China)
71
Optimization of Magnetic Field Configurations of a Miniature DC Ion Thruster with an Inverted Potential Structure
71
Optimization of Magnetic Field Configurations of a Miniature DC Ion Thruster with an Inverted Potential Structure
Speaker
Yoshinori Tanaka(Specialization in Aerospace Engineering，Graduate School of Engineering Science，Yokohama National University)
E-3
OS6: Electric Propulsion (3)
OS6: Electric Propulsion (3)
Details
Date
March Thu 16, 2023 14:20 - 16:00
Room
Room E
Chairperson
161
A Journey of Electric Propulsion Propellant -From Storage Tank to Vacuum Pump-
161
A Journey of Electric Propulsion Propellant -From Storage Tank to Vacuum Pump-
Speaker
Yoshinori Nakayama(National Defense Academy)
22
Performance Characteristics of Hall-Effect Thrusters for Transportation in the Solar System -Use of Carbon Dioxide, Methane, Ammonia, Hydrogen, Helium, Air and Ice/Water etc. in the Planets and Satellites to Propellants-
22
Performance Characteristics of Hall-Effect Thrusters for Transportation in the Solar System -Use of Carbon Dioxide, Methane, Ammonia, Hydrogen, Helium, Air and Ice/Water etc. in the Planets and Satellites to Propellants-
Speaker
Takuya Nakajima(Osaka Sangyo University)
242
Iodine-fed hollow cathode discharge: Insights gained from computer modeling
242
Iodine-fed hollow cathode discharge: Insights gained from computer modeling
Speaker
Ran Liu(School of Astronautics, Beihang University)
21
Performance Characteristics of Steady-State Axial-Magnetic-Field MPD Thrusters for Transportation in the Solar System -Use of Carbon Dioxide, Methane, Ammonia, Hydrogen, Helium, Air and Water/Ice etc. in the Planets and Satellites to Propellants-
21
Performance Characteristics of Steady-State Axial-Magnetic-Field MPD Thrusters for Transportation in the Solar System -Use of Carbon Dioxide, Methane, Ammonia, Hydrogen, Helium, Air and Water/Ice etc. in the Planets and Satellites to Propellants-
Speaker
Yuta Nanri(Osaka Sangyo University)
E-4
OS6: Electric Propulsion (4)
OS6: Electric Propulsion (4)
Details
Date
March Thu 16, 2023 16:20 - 18:00
Room
Room E
Chairperson
30
Thrust Performance and Their Enhancement of Direct-Current Arcjet Thrusters -Use of Carbon Dioxide, Methane, Ammonia, Hydrogen, Helium, Air and Ice/Water etc. in Planets and Satellites in the Solar System to Propellants-
30
Thrust Performance and Their Enhancement of Direct-Current Arcjet Thrusters -Use of Carbon Dioxide, Methane, Ammonia, Hydrogen, Helium, Air and Ice/Water etc. in Planets and Satellites in the Solar System to Propellants-
Speaker
Yui Sasai(Osaka Sangyo University)
4
Discharge Control Experiments of a SF-MPD Thruster using IGBT
4
Discharge Control Experiments of a SF-MPD Thruster using IGBT
Speaker
Kazuma Ueno(Chukyo University)
237
Spectroscopic measurement and simulation analysis of tungsten cathode erosion rate in an argon plasma arc
237
Spectroscopic measurement and simulation analysis of tungsten cathode erosion rate in an argon plasma arc
Speaker
Xing Han(Beihang university)
233
3-D measurements of the current density flux in a pulsed plasma thruster
233
3-D measurements of the current density flux in a pulsed plasma thruster
Speaker
Zhe Zhang(Beijing Institute of Technology, School of Aerospace Engineering)
92
Performance Evaluation of a Plasma Thruster Using High Temperature Superconducting Magnet
92
Performance Evaluation of a Plasma Thruster Using High Temperature Superconducting Magnet
Speaker
Kiyoshi Kinefuchi(Nagoya University)
E-5
OS6: Electric Propulsion (5)
OS6: Electric Propulsion (5)
Details
Date
March Fri 17, 2023 08:40 - 10:20
Room
Room E
Chairperson
145
Magnetic nozzle radiofrequency plasma thruster
145
Magnetic nozzle radiofrequency plasma thruster
Speaker
Takahashi Kazunori(Department of Electrical Engineering, Tohoku University)
14
Study on electromagnetic acceleration and thrust generation by air plasma for air breathing electric propulsion
14
Study on electromagnetic acceleration and thrust generation by air plasma for air breathing electric propulsion
Speaker
Masanori Harada(Kanazawa institute of technology)
212
Evaluation of electron energy probability function in an RF plasma thruster using a single helical antenna
212
Evaluation of electron energy probability function in an RF plasma thruster using a single helical antenna
Speaker
Furukawa Takeru(Kobe University，Department of Electrical and Electronic Engineering)
231
A novel and efficient dual-antenna micro plasma thruster
231
A novel and efficient dual-antenna micro plasma thruster
Speaker
Lei Chang(Institute of Plasma Physics, Chinese Academy of Sciences)
E-6
OS6: Electric Propulsion (6)
OS6: Electric Propulsion (6)
Details
Date
March Fri 17, 2023 10:40 - 12:00
Room
Room E
Chairperson
101
Ionic Liquid Electrospray Thrusters with Different Types of Emitter Structures
101
Ionic Liquid Electrospray Thrusters with Different Types of Emitter Structures
Speaker
Yoshinori Takao(Yokohama National University)
236
Roll torque measurement and interpretation of low power Hall-effect thrusters
236
Roll torque measurement and interpretation of low power Hall-effect thrusters
Speaker
Zhongkai Zhang(Beihang University)
251
Experimental Studies on Taylor Cone Formation and Ionization with Annular Slit Type Emitter for FEEP Thruster
251
Experimental Studies on Taylor Cone Formation and Ionization with Annular Slit Type Emitter for FEEP Thruster
Speaker
Chanearl Kwon(Seoul National University)
E-7
OS6: Electric Propulsion (7)
OS6: Electric Propulsion (7)
Details
Date
March Fri 17, 2023 13:00 - 14:20
Room
Room E
Chairperson
142
Particle analysis of electron cooling and ion acceleration in a magnetic nozzle thruster
142
Particle analysis of electron cooling and ion acceleration in a magnetic nozzle thruster
Speaker
Kazuma Emoto(Yokohama National University，Japan Society for the Promotion of Science)
211
Analysis of Wall Erosion of a Hall thruster Using Fluid-Particle Simulation
211
Analysis of Wall Erosion of a Hall thruster Using Fluid-Particle Simulation
Speaker
Gwanyong Jung(Korea Aerospace University)
31
Development of Commercially-Available High-Impulse Electrothermal Pulsed Plasma Thruster Systems in Osaka Sangyo University -from Charging Electric Energy/Power: 1J/1W for 1U(1kg) Cubesats to 50J/50W for 50cm Cube (50kg) Nano-Satellites-
31
Development of Commercially-Available High-Impulse Electrothermal Pulsed Plasma Thruster Systems in Osaka Sangyo University -from Charging Electric Energy/Power: 1J/1W for 1U(1kg) Cubesats to 50J/50W for 50cm Cube (50kg) Nano-Satellites-
Speaker
Yoshihiro Takakuwa(Osaka Sangyo University)
29
Development of Osaka Sangyo University 1U Cubesat OSU-1 with 1J/1W Pulsed Plasma Thruster Systems for Powered Flight, and R&D Project of Nano-Satellites/ Probes OSU-2, 3 and 4
29
Development of Osaka Sangyo University 1U Cubesat OSU-1 with 1J/1W Pulsed Plasma Thruster Systems for Powered Flight, and R&D Project of Nano-Satellites/ Probes OSU-2, 3 and 4
Speaker
Renichiro Oka(Osaka Sangyo University)
E-8
OS6: Electric Propulsion (8)
OS6: Electric Propulsion (8)
Details
Date
March Fri 17, 2023 14:40 - 16:00
Room
Room E
Chairperson
176
Multimode propulsion application for collision avoidances and drag-compensation: mission analysis and lifecycle value
176
Multimode propulsion application for collision avoidances and drag-compensation: mission analysis and lifecycle value
Speaker
Hiroyuki Koizumi(The University of Tokyo)
213
Estimation of On-orbit Potential Difference between Spacecraft and Ion Thruster Plume for Hayabusa2 by Analysis of Its Surface Erosion Near the Thruster
213
Estimation of On-orbit Potential Difference between Spacecraft and Ion Thruster Plume for Hayabusa2 by Analysis of Its Surface Erosion Near the Thruster
Speaker
Takanobu Muranaka(Chukyo University)
240
10,000 seconds-level micro-Newton thrust measurement utilizing superconducting magnetic levitated teststand and its noise characteristics
240
10,000 seconds-level micro-Newton thrust measurement utilizing superconducting magnetic levitated teststand and its noise characteristics
Speaker
Fuwen Deng(Beihang University)
106
Feasibility studies for two types of air-breathing ion engine with different ion source geometries.
106
Feasibility studies for two types of air-breathing ion engine with different ion source geometries.
Speaker
Yukai Miya(The Graduate University for Advanced Studies, SOKENDAI)
F-1
Fluid Dynamics (1)
Fluid Dynamics (1)
Details
Date
March Thu 16, 2023 08:20 - 10:20
Room
Room F
Chairperson
248
Performance Characteristics of Steam Turbine Cascade with Non-Equilibrium Condensation
248
Performance Characteristics of Steam Turbine Cascade with Non-Equilibrium Condensation
Speaker
Esmail Lakzian(Andong National University，Hakim Sabzevari University)
78
Acceleration of Large-Eddy Simulation for Slowly Pulsating Flows Using Harmonic Balance Approach
78
Acceleration of Large-Eddy Simulation for Slowly Pulsating Flows Using Harmonic Balance Approach
Speaker
Yuma Iwamoto(the University of Tokyo)
80
A Study on performance change of compressor and turbine due to blades wear caused by sand erosion for an aircraft turbofan engine.
80
A Study on performance change of compressor and turbine due to blades wear caused by sand erosion for an aircraft turbofan engine.
Speaker
Sooin Jeong(Pusan National University)
137
Effects of axial position and stagger angle errors on performance and stability of axial compressors
137
Effects of axial position and stagger angle errors on performance and stability of axial compressors
Speaker
zhengtao Guo(Northwestern Polytechnical University)
199
Development of Extended Redlich-Kwong-Peng-Robinson Equation of State
199
Development of Extended Redlich-Kwong-Peng-Robinson Equation of State
Speaker
Jiwan Seo(Seoul National University，Department of Aerospace Engineering)
40
The pre-swirl effect on the stall precursor of vaned diffuser inside a 1.5-stage centrifugal compressor
40
The pre-swirl effect on the stall precursor of vaned diffuser inside a 1.5-stage centrifugal compressor
Speaker
Xiaohuan Gao(Xi’an Jiaotong University)
F-2
Fluid Dynamics (2)
Fluid Dynamics (2)
Details
Date
March Thu 16, 2023 10:40 - 12:20
Room
Room F
Chairperson
50
Extension of a harmonic balance method to the incoming wake effect on the separated boundary layer
50
Extension of a harmonic balance method to the incoming wake effect on the separated boundary layer
Speaker
Shun Nakamura(Department of Aeronautics and Astronautics. University of Tokyo)
139
Mechanism investigation on the influence of inlet distortion on the aerodynamic performance of compressor
139
Mechanism investigation on the influence of inlet distortion on the aerodynamic performance of compressor
Speaker
Song Yan(School of Power and Energy, Northwest Polytechnical University)
166
The Effects of the Blade Loading Redistribution on the Performance of a Vaneless Counter-Rotating Turbine
166
The Effects of the Blade Loading Redistribution on the Performance of a Vaneless Counter-Rotating Turbine
Speaker
Tiantian Dong(Institute of Engineering Thermophysics, CAS, Beijing, China，School of Aeronautics and Astronautics, UCAS, Beijing, China)
222
Numerical study on the effect of variable guide vanes(VGVs) actuator faults to the multi-stage axial compressor performance.
222
Numerical study on the effect of variable guide vanes(VGVs) actuator faults to the multi-stage axial compressor performance.
Speaker
Byoungik Choi(Pusan National University)
56
Thermo-Fluid-Structure Interaction Analysis on Transient Behavior of Compressor Rotor in Fast Start-Up Operation
56
Thermo-Fluid-Structure Interaction Analysis on Transient Behavior of Compressor Rotor in Fast Start-Up Operation
Speaker
Takushi Muto(The University of Tokyo)
F-3
Fluid Dynamics (3)
Fluid Dynamics (3)
Details
Date
March Thu 16, 2023 14:20 - 16:00
Room
Room F
Chairperson
66
Numerical investigation of unsteady film cooling characteristics on turbine blade squealer tip
66
Numerical investigation of unsteady film cooling characteristics on turbine blade squealer tip
Speaker
Yulong You(AECC COMMERCIAL AIRCRAFT ENGINE CO., LTD.)
134
Investigation on Using Passive Self-recirculation for Shock Wave/Boundary Layer Interaction Control in a Supersonic Compressor Cascade
134
Investigation on Using Passive Self-recirculation for Shock Wave/Boundary Layer Interaction Control in a Supersonic Compressor Cascade
Speaker
Xiaoxiao Zhou(Institute of Engineering Thermophysics, CAS，School of Aeronautics and Astronautics, UCAS)
181
Experimental Aerodynamic and Aeromechanic Investigation of a Transonic Axial Fan
181
Experimental Aerodynamic and Aeromechanic Investigation of a Transonic Axial Fan
Speaker
Byeungjun Lim(Korea Aerospace Research Institute)
49
Resolvent analysis for compressibility effect on jet share layer
49
Resolvent analysis for compressibility effect on jet share layer
Speaker
Daichi Ogawa(Department of Aeronautics and Astronautics)
F-4
Fluid Dynamics (4)
Fluid Dynamics (4)
Details
Date
March Thu 16, 2023 16:20 - 18:00
Room
Room F
Chairperson
132
Numerical analysis on heat transfer and pressure loss characteristics of flow boiling under ground gravity and microgravity
132
Numerical analysis on heat transfer and pressure loss characteristics of flow boiling under ground gravity and microgravity
Speaker
Yuki Miyara(The University of Tokyo)
95
Particle-grid hybrid analysis of liquid jet primary breakup in gaseous crossflow
95
Particle-grid hybrid analysis of liquid jet primary breakup in gaseous crossflow
Speaker
Hiroki Tsujimura(Waseda University)
25
Pressure-based semi-implicit solver considering real gas effect
25
Pressure-based semi-implicit solver considering real gas effect
Speaker
Sho Wada(Kyoto university)
7
Research on the effect of movable flaps with different modes on energy harvesting efficiency of a flapping wing
7
Research on the effect of movable flaps with different modes on energy harvesting efficiency of a flapping wing
Speaker
Chenye Tian(Xi An Jiaotong University)
202
A Numerical Study on NOx Formation in a Model Afterburner for a Hydrogen-fueled Pre-cooled Turbo Jet Engine with an Unsupervised Clustering Algorithm.
202
A Numerical Study on NOx Formation in a Model Afterburner for a Hydrogen-fueled Pre-cooled Turbo Jet Engine with an Unsupervised Clustering Algorithm.
Speaker
Kotaro Nakayama(The University of Tokyo)
F-5
Fluid Dynamics (5)
Fluid Dynamics (5)
Details
Date
March Fri 17, 2023 08:40 - 10:20
Room
Room F
Chairperson
183
The Oscillatory Behavior of Multiple Shock Waves in a Supersonic Duct
183
The Oscillatory Behavior of Multiple Shock Waves in a Supersonic Duct
Speaker
Jintu James(Department of Mechanical Engineering, Andong National University)
43
Contribution of a Hybrid NS-DSMC Methodology for Rarefied Jet Flow Simulations
43
Contribution of a Hybrid NS-DSMC Methodology for Rarefied Jet Flow Simulations
Speaker
Virgile Charton(Department of Aerospace Engineering, Nagoya University)
75
Influence of Gas Properties on Film Cooling Performances of a Turbine Vane Serviced in Fuel-Rich Gas Environment
75
Influence of Gas Properties on Film Cooling Performances of a Turbine Vane Serviced in Fuel-Rich Gas Environment
Speaker
Yutao Ma(Institute of Engineering Thermophysics, CAS，University of Chinese Academy of Sciences)
143
Analysis of vibrational energy transmission characteristics of the disk-shaft assembly induced to nonlinear contacts
143
Analysis of vibrational energy transmission characteristics of the disk-shaft assembly induced to nonlinear contacts
Speaker
shen liu(Institute of Engineering Thermophysics,CAS， University of Chinese Academy of Sciences)
174
Improvements of V-shaped vortex generator on film cooling performance
174
Improvements of V-shaped vortex generator on film cooling performance
Speaker
Wei Tian(Shanghai Jiao Tong University)
F-6
OS2: Hydrogen-Powered Aerospace Engines (1)
OS2: Hydrogen-Powered Aerospace Engines (1)
Details
Date
March Fri 17, 2023 10:40 - 12:00
Room
Room F
Chairperson
23
Design Study on Hydrogen Jet Research Engine for Hydrogen-Powered Aircraft
23
Design Study on Hydrogen Jet Research Engine for Hydrogen-Powered Aircraft
Speaker
HIDEYUKI TAGUCHI(Japan Aerospace Exploration Agency)
46
Development of Liquid hydrogen powered electric propulsion system
46
Development of Liquid hydrogen powered electric propulsion system
Speaker
Kiyoto Fujimatsu(IHI AEROSPACE，Technologies Development Office)
82
A study on FGM method considering preferential diffusion for numerical simulation of hydrogen/air premixed flame
82
A study on FGM method considering preferential diffusion for numerical simulation of hydrogen/air premixed flame
Speaker
Kai Reo(Kyoto University)
83
Combustion Conditions of Hydrogen Lifted flame formed on the injector diameter less than 1 mm
83
Combustion Conditions of Hydrogen Lifted flame formed on the injector diameter less than 1 mm
Speaker
Kazunori Ichieda(Graduate School of Systems Design, Tokyo Metropolitan University)
F-7
OS2: Hydrogen-Powered
OS2: Hydrogen-Powered
Details
Date
March Fri 17, 2023 13:00 - 14:20
Room
Room F
Chairperson
87
Boiling Heat Transfer Enhancement of Piping System for Cryogenic Fuel
87
Boiling Heat Transfer Enhancement of Piping System for Cryogenic Fuel
Speaker
Katsuyoshi Fukiba(Shizuoka University)
98
Effect of increased equivalence ratio on combustion instability of premixed hydrogen flames in low-swirl combustor
98
Effect of increased equivalence ratio on combustion instability of premixed hydrogen flames in low-swirl combustor
Speaker
Jun Nagao(Kyoto University)
102
Conceptual Design Study of Liquid Hydrogen Aircraft Incorporating Hydrogen Fuel Propulsion Model and Aircraft Conceptual Design Tool
102
Conceptual Design Study of Liquid Hydrogen Aircraft Incorporating Hydrogen Fuel Propulsion Model and Aircraft Conceptual Design Tool
Speaker
Kotaro Kikuchi(The University of Tokyo)
91
Thermal Performance of a Low-Pressure Cryogenic Vaporizer for Liquified Hydrogen
91
Thermal Performance of a Low-Pressure Cryogenic Vaporizer for Liquified Hydrogen
Speaker
SeoYeon Kang(Korea Aerospace University，Department of Aerospace and Mechanical University，Department of Smart Air Mobility)
F-8
OS2: Hydrogen-Powered Aerospace Engines (3)
OS2: Hydrogen-Powered Aerospace Engines (3)
Details
Date
March Fri 17, 2023 14:40 - 16:00
Room
Room F
Chairperson
48
Analytical investigation on combustion instability in a hydrogen-fueled gas turbine combustor.
48
Analytical investigation on combustion instability in a hydrogen-fueled gas turbine combustor.
Speaker
SMZohairHussain Shah(Gangneung-Wonju National Univeristy, South Korea，Energy and Power System Lab)
207
Hydrogen combustion behaviors in a super Rich burn, Quick mix, Lean burn combustor of aircraft engine for lowering NOx emission
207
Hydrogen combustion behaviors in a super Rich burn, Quick mix, Lean burn combustor of aircraft engine for lowering NOx emission
Speaker
Daiki Ito(University of Tokyo)
124
Dependence of cavitation on inducer diameter and tip clearance
124
Dependence of cavitation on inducer diameter and tip clearance
Speaker
Shunsuke Sugimoto(The University of Tokyo)
122
Overviews of activities around enabling Hydrogen Aircraft
122
Overviews of activities around enabling Hydrogen Aircraft
Speaker
Hiroko Nakamura(The University of Tokyo)
L-1
Plenary Lecture
Plenary Lecture
Details
Date
March Thu 16, 2023 13:20 - 14:10
Room
Room A
Chairperson
247
Sounding-Rocket Space Flight Experiments of Detonation Engine System
247
Sounding-Rocket Space Flight Experiments of Detonation Engine System
Speaker
Jiro Kasahara(Nagoya University)
L-2
Keynote Speech
Keynote Speech
Details
Date
March Fri 17, 2023 16:20 - 18:20
Room
Room A
Chairperson
252
Innovative Research on Core-Technology of Hydrogen Aircraft for Realization of the Carbon Neutral Society
252
Innovative Research on Core-Technology of Hydrogen Aircraft for Realization of the Carbon Neutral Society
Speaker
YASUHIRO KINOSHITA(Exective Fellow，Hydrogen Aircraft Technology，Aerospace Systems Company，Kawasaki Heavy Industriles, Ltd.)