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
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
Speaker
Shoya Takeshi(Nihon university)
125 Study on Anomaly Detection of a Spacecraft Propulsion System using Machine Learning
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
Speaker
Jaehyun Nam(Department of Aerospace Engineering, Seoul National University)
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)
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)
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
Speaker
Keiichi OKAI(Japan Aerospace Exploration Agency)
206 Design Study of SOFC/Gas Turbine Combined Cycle Propulsion
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
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
Speaker
SeungMin Jeong(Pusan National University)
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)
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-
Speaker
Takuya Nakajima(Osaka Sangyo University)
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-
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
Speaker
Kazuma Ueno(Chukyo University)
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
Speaker
Zhe Zhang(Beijing Institute of Technology, School of Aerospace Engineering)
92 Performance Evaluation of a Plasma Thruster Using High Temperature Superconducting Magnet
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
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-
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
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
Speaker
Takanobu Muranaka(Chukyo University)
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.
Speaker
Yukai Miya(The Graduate University for Advanced Studies, SOKENDAI)
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
Speaker
Hiroki Tsujimura(Waseda University)
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
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.