Results 151 to 160 of about 28,421 (204)
Some of the next articles are maybe not open access.
2015
Abstract The chapter starts its analysis with blunt-nosed bodies. In a supersonic flow, a blunt-nosed body produces a bow shock wave. The chapter shows that the shape of the shock and the entire flow between the shock and the body become independent of the Mach number, M∞, provided it is large enough.
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Abstract The chapter starts its analysis with blunt-nosed bodies. In a supersonic flow, a blunt-nosed body produces a bow shock wave. The chapter shows that the shape of the shock and the entire flow between the shock and the body become independent of the Mach number, M∞, provided it is large enough.
openaire +1 more source
Review of control and guidance technology on hypersonic vehicle
Chinese Journal of Aeronautics, 2022Xiaokui Yue +2 more
exaly
Analysis of Associative Ionization Rates for Hypersonic Flows
Journal of Thermophysics and Heat Transfer, 2021Iain Boyd, Eswar Josyula
exaly
INTERACTIONS BETWEEN A HYPERSONIC WAKE AND A FOLLOWING HYPERSONIC PROJECTILE
AIAA Journal, 1963R. E. SLATTERY +2 more
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Wall Pressure Fluctuations Beneath Hypersonic Boundary Layer over Plate
AIAA Journal, 2021Xiaojian Zhao
exaly
Research progress on active thermal protection for hypersonic vehicles
Progress in Aerospace Sciences, 2020Silong Zhang, Wen Bao, Jiang Qin
exaly
Review of acoustic metasurfaces for hypersonic boundary layer stabilization
Progress in Aerospace Sciences, 2022Juanmian Lei, Chih-Yung Wen, Rui Zhao
exaly
Review of combustion stabilization for hypersonic airbreathing propulsion
Progress in Aerospace Sciences, 2020Damiano Baccarella +2 more
exaly