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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On upstream influence in supersonic flows [PDF]
, 2005 The general problem of propagation of three-dimensional disturbances in viscous supersonic flows is considered in the framework of characteristic analysis.
Krechetnikov, R., Lipatov, I. I.
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Inviscid Hypersonic Flow Over Blunt-Nosed Slender Bodies [PDF]
, 1957 LESTER LEES, TOSHI KUBOTA
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Viscous shock layer solutions for turbulent flow of radiating gas mixtures in chemical equilibrium [PDF]
The viscous shock layer equations for hypersonic laminar and turbulent flows of radiating or nonradiating gas mixtures in chemical equilibrium are presented for two-dimensional and axially symmetric flow fields.
Anderson, E. C., Moss, J. N.
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Hypersonic aerodynamics on thin bodies with interaction and upstream influence [PDF]
, 1994 In the fundamental configuration studied here, a steady hypersonic free stream flows over a thin sharp aligned airfoil or flat plate with a leading-edge shock wave, and the flow field in the shock layer (containing a viscous and an inviscid layer) is ...
Khorrami, AF, Smith, FT
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Multigrid for hypersonic inviscid flows [PDF]
The use of multigrid methods to solve the Euler equations for hypersonic flow is discussed. The steady state equations are considered with a Runge-Kutta smoother based on the time accurate equations together with local time stepping and residual ...
Decker, Naomi H., Turkel, Eli
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Hypersonic Flows for Reentry Problems [PDF]
, 1991 INRIA and GAMNI/SMAI have organized a Workshop open to the international scientific community on hypersonic flows for reentry problems which was held in Palais des Congres d'Antibes in January 1990 (part I) and April 1991 (part II). This workshop was focussed on the issues of validation of numerical methodolies for the computation of high-Mach number ...
Jacques Periaux +2 more
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Asymmetric hypersonic flow [PDF]
A general method for the analysis of the inviscid asymmetric hypersonic flow fields enveloping smooth bodies of general shape is given. The method is based on the assumption of a thin shock layer which yields an expression for pressure in generalized ...
Maslen, S. H.
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Research on the drag reduction performance induced by the counterflowing jet for waverider with variable blunt radii [PDF]
, 2016 Waverider will endure the huge aero-heating in the hypersonic flow, thus, it need be blunt for the leading edge. However, the aerodynamic performance will decrease for the blunt waverider because of the drag hoik.
Barakos, George N. +4 more
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Some aspects of hypersonic flow over power law bodies [PDF]
, 1969 H. G. Hornung
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