Numerical Study of Turbulent Combustion in High Mach Number Scramjet Engine with Thermodynamic Non-equilibrium Effect
Hai FENG, Tai JIN, Kun WU
DOI Number: XXX-YYY-ZZZ
Conference number: HiSST2024-00328
The Current Status of Free-Flight Testing of a Scramjet-Integrated Hypersonic Cruising Vehicle Model in the HIEST Free-Piston Shock Tunnel
Hideyuki TANNO, Shuto YATSUYANAGI, Kouichiro TANI, Sadatake TOMIOKA
DOI Number: 10.60853/49rx-w175
Conference number: HiSST-2024-00326
Sensitivity Derivatives of a Low-Order Integrated Scramjet Propulsion Model for Gradient-Based Co-Design MDAO
Amir MITTELMAN, Kieran MACKLE, Ingo JAHN, Rowan GOLLAN
DOI Number: 10.60853/bpzq-f253
Conference number: HiSST-2024-00323
Achieving Optimal Designs for High-Speed Blunt Body vehicles: A Multi-Objective Approach with an Efficient Aerothermodynamic Prediction Program
Hoonjung YEO, Kyu Hong KIM
DOI Number: XXX-YYY-ZZZ
Conference number: HiSST2024-00322
Nozzle Flow Characterization of the SNU Hypersonic Shock Tunnel
Jinyoung KIM, Jinhwi KIM, Jungmu HUR, Bok Jik LEE, In Seuck JEUNG
DOI Number: XXX-YYY-ZZZ
Conference number: HiSST2024-00321
Acoustic Shock Wave-induced Phase Transition of Indium Selenide from Orthorhombic to Rhombohedral Crystal System
S. A Martin BRITTO DHAS, S. OVIYA, F. IRINE MARIA BINCY, Ikhyun KIM
DOI Number: 10.60853/6ftm-3553
Conference number: HiSST-2024-00319
Reduction of Pressure Load and Heat Load by Counter-flow Jet on a Blunt Body in Hypersonic Flow
Min Su HWANG, Hyoung Jin LEE
DOI Number: XXX-YYY-ZZZ
Conference number: HiSST2024-00318
Exploratory Design and Evaluation of Alumina-Based Oxide/Oxide Ceramic Matrix Composite for Integrated Thermal Protection System Application
Vinh Tung LE, Abhendra K SINGH
DOI Number: XXX-YYY-ZZZ
Conference number: HiSST2024-00317
Design and Starting Study of the Adjustable Inward Turning Inlet at Ma1.5~7
Fuzhou LIU, Huacheng YUAN, Keyu ZHOU, Zhenggui ZHOU
DOI Number: 10.60853/39s2-kn63
Conference number: HiSST-2024-00315
Experiments on High Speed Air-Breathing Propulsion for Sustainable Supersonic Flight
Friedolin Tobias STRAUSS, Konstantin MANASSIS, Marius WILHELM, Christoph KIRCHBERGER
DOI Number: 10.60853/82dy-6032
Conference number: HiSST-2024-00314