Results 91 to 100 of about 72,125 (260)
Aiming at improving the range of wing-body combination aircraft at hypersonic flow conditions and exploring the application of morphing technology in hypersonic aircraft, morphing aircrafts with different morphing modes have been proposed.
Wuyu Peng +3 more
doaj +1 more source
The effect of thermal and chemical boundary conditions on the structure and chemical composition of the wake behind a 3D Mach 7 sphere-cone at an angle of attack of 5 degrees and an altitude of roughly 30,000 m is explored.
Matthew J. Satchell +2 more
doaj +1 more source
A high-order finite difference method was used to simulate the hypersonic flow field over a blunt cone with different height roughness elements. The unsteady flow field induced by pulse disturbances was analyzed and compared with that under continuous ...
Zhenqing Wang +4 more
doaj +1 more source
Numerical simulation of hypersonic flow with non-equilibrium chemical reactions around sphere
Yury Dobrov +3 more
openalex +2 more sources
Gas–thermal–solid coupling analysis of a hypersonic inflatable reentry and descent system [PDF]
Xu Cao +4 more
openalex +1 more source
Investigation of the Inverse Magnus Effect on a Rotating Sphere in Hypersonic Rarefied Flow
Explorations involving long-endurance and maneuvering flights in the upper atmosphere, as well as research on atmospheric entries of space debris or asteroids, call for a full understanding of hypersonic rarefied flows.
Yazhong Jiang +2 more
doaj +1 more source
Hypersonic test facility Patent [PDF]
Hypersonic test facility for studying ablation in models under high pressure and high ...
Buchanan, R. I. +3 more
core +1 more source
Investigation of hypersonic conic flows generated by a magnetoplasma light-gas gun equipped with Laval nozzle [PDF]
П. П. Храмцов +6 more
openalex +1 more source
Hypersonic Flow Theory and Hypersonic Aerodynamics [PDF]
Wallace D. Hayes +3 more
openaire +1 more source
Mixing Characteristics of Single/Dual Injection Configurations
To investigate the fuel injection and mixing issues in the scramjet combustor, three-dimensional multi-species compressible flow solver has been developed using high-resolution numerical schemes and SST k-ω turbulence model.
Liang ZHU, Ze XU, Shiyuan GAO, Jun SONG
doaj +1 more source

