Computation of thermochemical nonequilibrium flows around a simple and a double ellipse [PDF]
, 1991 The nonequilibrium viscous reactive flows over a simple and a double ellipse at a 30 degree angle of attack were computed. The geometry and the free stream conditions are given by INRIA/GAMNI/SMAI workshop test cases 6.2-2 and 6.2-4. The governing Navier-
C Park +7 more
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Influence of coolant multi-jets on heat reduction of nose cone with blunt spike at hypersonic flow. [PDF]
Sci Rep, 2022 Ghanbari M, Maddah S, Alinejad J.
europepmc +1 more source
Experimental aerothermodynamic research of hypersonic aircraft [PDF]
Wind tunnel tests were conducted to establish a benchmark experimental data base for a genetic hypersonic aircraft vehicle. Comprehensive measurements were made at Mach 7 to give flow visualization, surface pressure, surface convective heat transfer, and
Cleary, Joseph W.
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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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A review on the development of large-scale detonation-driven shock tunnels and the application in hypersonic flow tests [PDF]
International Journal of Fluid EngineeringWith the boom in deep space exploration by China since the beginning of the 21st century, the demand for high-enthalpy hypersonic shock tunnels has continued to increase.
Zongmin Hu, Wenhao Wang, Zijian Zhang
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Numerical study of lateral coolant jet on heat reduction over nose cone with double-aerodome at hypersonic flow. [PDF]
Sci Rep, 2022 Ghanbari M, Maddah S, Alinejad J.
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Flow field computations for blunt bodies in planetary environments [PDF]
Numerical analysis on flow distribution around hypersonic blunt body in planetary ...
Byron, S., Foster, R. M., Masson, B. S.
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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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An investigation of some effects of mach number and air temperature on the hypersonic flow over a blunt body [PDF]
Mach number and air temperature effect on hypersonic flow over blunt ...
Seiff, A., Sommer, S. C.
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Авіаційно-космічна техніка та технологіяThis study presents the main results of research on the assessment of the change in the influence of the adiabatic index on the total pressure conservation coefficient and the length of the direct compression jump in the supersonic part of the external ...
Artem Khorokhordin +1 more
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