Aeroelasticity of smart wing in supersonic flow
Reza Moosavi
DOI Number: https://doi.org/10.82439/ceas-ifasd-2024-139
Conference number: IFASD-2024-139
Design and Characterization of a 6-in High-enthalpy Impulse Test Facility
Youngjin JUN, Seongkyun IM
DOI Number: N/A
Conference number: HiSST-2024-278
Aerodynamics of the Reusable Launch Vehicle Supersonic Retropropulsion System
Jesslyn Wei Yan ONG, Yujoo KANG, Jaemyung AHN, Sang LEE
DOI Number: https://doi.org/10.82241/ceas-hisst-2024-249
Conference number: HiSST-2024-249
Simulation of the Mixing of a Supersonic Air Flow with a Transverse Jet under the Conditions of Pulse-periodic Local Heating
Aleksandr A. FIRSOV, Luka S. VOLKOV, Yakov V. Miroshnikov
DOI Number: N/A
Conference number: HiSST-2024-194
Properties of Direct Current Discharge in a Supersonic Flow, and Its Application for Plasma-Assisted Combustion
Aleksandr A. FIRSOV, Anastasia S. DOBROVOLSKAYA, Dmitriy A. TARASOV, Roman S. TROSHKIN, Valentin A. BITYURIN, Aleksey N. BOCHAROV
DOI Number: N/A
Conference number: HiSST-2024-193
Drag due to Distributed Roughness in Supersonic Turbulent Boundary Layers: Comparison between Experiments and Numerics
Quentin CHANZY, Sylvain MORHILAT, Antoine DURANT, Vincent BRION
DOI Number: https://doi.org/10.82241/ceas-hisst-2024-182
Conference number: HiSST-2024-182
Direct Numerical Simulation of Strong Shock-turbulent Boundary Layer Interaction
Yujoo KANG, Sang LEE
DOI Number: https://doi.org/10.82241/ceas-hisst-2024-170
Conference number: HiSST-2024-170
Aero-Thermal Study and Experimental Characterization of a Novel Optical Probe for High Temperature Supersonic Flows
Ignacio LASALA AZA, Aubrey MCKELVY, Guillermo PANIAGUA-PEREZ, Etienne CHOQUET, Thierry ANDRÉ, François FALEMPIN
DOI Number: https://doi.org/10.82241/ceas-hisst-2024-154
Conference number: HiSST-2024-154
Shock Wave Structure and Surface Pressure Prediction using Deep Learning Model
Min Hyun HAN, Soo Hyung PARK
DOI Number: N/A
Conference number: HiSST-2024-045
Experimental measurements on Tekna’’PlasmaSonic’’ High EnthalpyGround Testing Facilities using 350 kW ICPT plasma torch to reproduce re-entry conditions of space vehicles
Y. Lakaf, S. Xue
DOI Number XXX-YYY-ZZZ
Conference Number HiSST-2022-0404