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Hypersonic Flow Around a Sphere
Journal of the Aerospace Sciences, 1958a, b, c D f constants, Eq. (9) diameter of the sphere function of d function of r Poo/ps p = pressure r — radial coordinate, distance from center of sphere R = shock radius, radial coordinate of shock u = radial component of velocity £7 oo = free-stream velocity v = circumferential component of velocity 8 = (2/D)V'Q _ Q , stagnation-point surface ...
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Introduction to Hypersonic Flows
2015In the previous chapters, compressibility effects are covered, particularly in the transonic regime where the Mach number is close to one.
J. J. Chattot, M. M. Hafez
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Physics Bulletin, 1959
By W. D. Hayes and R. F. Probstein New York and London: Academic Press Inc. Pp. xiv + 464. Price 92s. The book is directed to students and research workers in the field of modern gas-dynamics and to hypersonic aerodynamicists. The authors divide the hypersonic features of a high speed flow into those of a " hydrodynamic " nature which arise because the
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By W. D. Hayes and R. F. Probstein New York and London: Academic Press Inc. Pp. xiv + 464. Price 92s. The book is directed to students and research workers in the field of modern gas-dynamics and to hypersonic aerodynamicists. The authors divide the hypersonic features of a high speed flow into those of a " hydrodynamic " nature which arise because the
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Nature, 1960
Hypersonic Flow Theory By Wallace D. Hayes and Ronald F. Probstein. (Applied Mathematics and Mechanics, Vol. 5. Series of Monographs prepared under the auspices of the Applied Physics Laboratory, The Johns Hopkins University.) Pp. xiv + 464. (New York: Academic Press, Inc.; London: Academic Press, Inc. (London), Ltd., 1959.) 11.50 dollars.
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Hypersonic Flow Theory By Wallace D. Hayes and Ronald F. Probstein. (Applied Mathematics and Mechanics, Vol. 5. Series of Monographs prepared under the auspices of the Applied Physics Laboratory, The Johns Hopkins University.) Pp. xiv + 464. (New York: Academic Press, Inc.; London: Academic Press, Inc. (London), Ltd., 1959.) 11.50 dollars.
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1969
At hypersonic Mach numbers, significant pressures are induced on aerodynamic surfaces by both viscosity and bluntness effects. Viscosity-induced pressures are caused by the growth of the boundary layer. They are accounted for in the manner proposed by Prandtl (1) many years ago when he suggested taking the computed boundary-layer displacement thickness
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At hypersonic Mach numbers, significant pressures are induced on aerodynamic surfaces by both viscosity and bluntness effects. Viscosity-induced pressures are caused by the growth of the boundary layer. They are accounted for in the manner proposed by Prandtl (1) many years ago when he suggested taking the computed boundary-layer displacement thickness
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Two−dimensional hypersonic magnetohydrodynamic flow
The Physics of Fluids, 1975The problem of the two−dimensional, inviscid, infinitely−conducting hypersonic flow past nonconducting bodies, in the presence of near−aligned magnetic fields, is analyzed, the problem being solved by transforming from the physical plane to the stream function, magnetic stream function plane.
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Temporal characteristics of hypersonic flows over a double wedge with Reynolds number
Physics of Fluids, 2023Özgur Tumuklu, Kyle M Hanquist
exaly