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Author: Donald Louis Baradell
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 54
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Book Description
Author: Donald Louis Baradell
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 54
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Book Description
Author: Donald L. Baradell
Publisher:
ISBN:
Category :
Languages : en
Pages : 60
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Author: Norbert Andrew Durando
Publisher:
ISBN:
Category :
Languages : en
Pages : 212
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Book Description
Author: Marcus O. Creager
Publisher:
ISBN:
Category : Numerical analysis
Languages : en
Pages : 32
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Book Description
Author: Davis H. Crawford
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 68
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Book Description
Author: George David Katz
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 164
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Author: C. C. Horstman
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Author: G. M. Gregorek
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 124
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Book Description
Vol. 1 Pressures were measured over the surface of an unswept blunt flat plate having a cylindrical leading edge 1/2-inch in diameter. The flat plate was side-mounted in the ALOSU 12-inch continuous hypersonic wind tunnel. Separate tests were conducted with cylinders in order to obtain detailed data for the leading-edge. Stagnation temperatures were sufficiently high to eliminate condensation effects. The leading edge and cylinder pressure ratios were noted to be independent of both Mach number and Reynolds number. The flat plate pressure ratios show a small dependence on Mach number. Reynolds number effects on the plate pressure ratios were small except at the lower levels of Reynolds number where the interaction of the thickened boundary layer caused increases in pressure.
Author: HakurÅ Oguchi
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 1
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Study was made of the hypersonic flow over a flat plate with a blunt nose. The analysis is based on the flow model in which the flow field behind the shock wave may be divided into two regions: (1) the inviscid-hypersonic-flow region and (2) the entropy layer, across which the pressure undergoes no appreciable change. (Author).
Author: Michael E. Tauber
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44
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