Aerospace, 2018 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
Ramjet Nozzle Analysis for Transport Aircraft Configuration for Sustained Hypersonic Flight
Applied Sciences, 2018 For the past several decades, research dealing with hypersonic flight regimes has been restricted mainly to military applications. Hypersonic transportation could be a possible and affordable solution to travel in the medium term and there is renewed ...
Raman Baidya +2 more
doaj +1 more source
Investigation of the Inverse Magnus Effect on a Rotating Sphere in Hypersonic Rarefied Flow
Applied SciencesExplorations 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
Inviscid Hypersonic Flow Over Blunt-Nosed Slender Bodies [PDF]
, 1957 LESTER LEES, TOSHI KUBOTA
openalex +1 more source
Universal behavior of internal friction in glasses below T : anharmonicity vs relaxation
, 2006 Comparison of the internal friction at hypersonic frequencies between a few K and the glass transition temperature Tg for various glasses brings out general features. At low temperature, internal friction is only weakly dependent on the material. At high
C. A. Angell +18 more
core +2 more sources
EFFECTS OF COOLING ON TRANSITION IN THE BOUNDARY LAYER ON A HEMISPHERE IN SIMULATED HYPERSONIC FLOW [PDF]
, 1961 Roger A. Dunlap, Arnold M. Kuethe
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A Microwave Method of determining the Displacement and Velocity of a Piston in a Hypersonic Gun Tunnel [PDF]
, 1959 L. Pennelegion
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Mixing Characteristics of Single/Dual Injection Configurations
气体物理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
Shock-Wave Effects on the Laminar Skin Friction of an Insulated Flat Plate at Hypersonic Speeds [PDF]
, 1953 Ting-Yi Li, H. T. Nagamatsu
openalex +1 more source
High speed flight vehicle control Patent [PDF]
, 1971 Supersonic or hypersonic vehicle control system comprising elevons with hinge line sweep and free of adverse aerodynamic cross ...
Rainey, R. W.
core +1 more source