The Flow about the Leading Edge of a Swept Blunt Plate at Hypersonic Speeds PDF Download
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Author: C. C. Horstman
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 36
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Book Description
Author: C. C. Horstman
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 36
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Book Description
Author: C. C. Horstman
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 0
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Book Description
As part of a fundamental study of hypersonic wings, some detailed pressure distribution and heat transfer results were obtained over sections of the leading edge region of a blunt plate at sweep angles from zero to 75 degrees. The tests were carried out in a Helium hypersonic wind tunnel at Mach numbers from 7 to 17. Some effects of the apex or upstream boundary of the plate on the leading edge regions under study were determined at various stations along the leading edge. The leading edge regions examined showed deviations from normal Mach number considerations at high sweep angles over the entire Mach number range studied.
Author: John D. Lee
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
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Over wide ranges in Mach number, sweep angle and attack angle, simple adjusted forms of Newtonian, Prandtl-Meyer, and blast wave theories may be used to accurately predict the pressure distributions on blunt-edged flat plates, in cluding the leading edge regions. On the leading edge, Newtonian-Prandtl-Meyer flow may be adjusted with an empirical factor to fit available experimental data. For the plate surface, the blast wave equation is modified by matching to the pressures at the cylinder-plate junction and on the infinite wedge, corresponding to the proper sweep and attack angle. (Author).
Author:
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ISBN:
Category :
Languages : en
Pages : 488
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 836
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Author: Ronald C. Smith
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 36
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Author: James R. Batt
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 392
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Author: United States. Wright Air Development Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1276
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Author: Edward J. Hopkins
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 36
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Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 568
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