STUDIES OF MICROWAVE TRANSMISSION THROUGH A HYPERSONIC AIR PLASMA. Final Report, June 1967.
, 1968 D. W. Boyer, G. Bein, S.N. Andre
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Engineering aerodynamic heating method for hypersonic flow [PDF]
, 1992 Christopher J. Riley, Fred R. DeJarnette
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Application of a Gas-Kinetic BGK Scheme in Thermal Protection System Analysis for Hypersonic Vehicles. [PDF]
Entropy (Basel), 2022 Zhou D, Du B, Guo T, Li Q, Lu Z.
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Spatial evolution of nonlinear acoustic mode instabilities on hypersonic boundary layers [PDF]
, 1990 M. E. Goldstein, David W. Wundrow
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Gas Kinetic Scheme Coupled with High-Speed Modifications for Hypersonic Transition Flow Simulations. [PDF]
Entropy (Basel)Li C +5 more
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Influence of lateral single jets for thermal protection of reentry nose cone with multi-row disk spike at hypersonic flow: computational study. [PDF]
Sci Rep, 2023 Shi Y +6 more
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HEAT TRANSFER AND FLOW VISUALIZATION ON 1/2-INCH-DIAMETER CYLINDERS IN LAMINAR HYPERSONIC FLOW
, 1966 Not Given Author
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Hypersonic aerodynamics on thin bodies with interaction and upstream influence [PDF]
, 1994 A. Farid Khorrami, F. T. Smith
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Thermal modal analysis of hypersonic composite wing on transient aerodynamic heating. [PDF]
Sci RepWang K +5 more
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A DIGITAL PITCHING SECTOR CONTROL SYSTEM FOR THE SANDIA 18-INCH HYPERSONIC WIND TUNNEL.
, 1967 D.R. MacKenzie
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