Observation of Hydrogen Combustion Characteristics in a Scramjet Combustor Based on Cavity Type
Geon Wook YIM, Hyoung Jin LEE
DOI Number: XXX-YYY-ZZZ
Conference number: HiSST2024-00180
Investigation on the Linear Stationary Crossflow Stability Characteristics of Hypersonic Boundary Layer with Expansion Corner
Peisen LU, Youcheng XI, Song FU
DOI Number: 10.60853/452e-0006
Conference number: HiSST-2024-00179
Experimental Study on Thermal Decomposition Characteristics of exo-THDCPD
Seung Mook PARK, Seung Hyeon LEE, Hyung Ju LEE
DOI Number: XXX-YYY-ZZZ
Conference number: HiSST2024-00178
Measurement Method of Thermal Environment of Reentry Capsule
Guangsen JIA, Dapeng YAO, Xin JIN, Jian LIN, Nong CHEN
DOI Number: 10.60853/4gms-kh33
Conference number: HiSST-2024-00177
Heat Flux Increment Induced by the Coupled Shear and Compression Effects in Laminar Hypersonic Flows
Huijun GAO, Zhi hui WANG
DOI Number: XXX-YYY-ZZZ
Conference number: HiSST2024-00175
Investigation of Detonation Wave Phenomena in Non-Premixed H2-AirAnnular Rotating Detonation Combustor using Large-Eddy Simulation
Yuxiang LIM, Thommie NILSSON, Christer FUREBY
DOI Number: XXX-YYY-ZZZ
Conference number: HiSST2024-00174
Theoretical Analysis of Interaction between Rotating Detonation Wave and Upstream Flow Field
Sijia Gao, Han Peng, Yue Huang, Zhipeng Sun, Yancheng You
DOI Number: XXX-YYY-ZZZ
Conference number: HiSST2024-00173
A Design Method for All-movable Rudder Structure with Lattices and Stiffeners by Thermo-elastic Topology Optimization under Mass Constraints
Yang LI, Tong GAO
DOI Number: XXX-YYY-ZZZ
Conference number: HiSST2024-00172
Direct Numerical Simulation of Strong Shock-turbulent Boundary Layer Interaction
Yujoo KANG, Sang LEE
DOI Number: 10.60853/qa87-wp92
Conference number: HiSST-2024-00170
Experimental Measurements on Tekna’’PlasmaSonic’’ High Enthalpy Ground Testing Facilities using 350 kW ICPT Plasma Torch to Reproduce Re-entry Conditions of Space Vehicles
Yazid LAKAF, Siwen XUE, Eric BOUCHARD
DOI NUmber: XXX-YYY-ZZZ
Conference number: HiSST 2024-00168