The Flow about the Leading Edge of a Swept Blunt Plate at Hypersonic Speeds PDF Download

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The Flow about the Leading Edge of a Swept Blunt Plate at Hypersonic Speeds

The Flow about the Leading Edge of a Swept Blunt Plate at Hypersonic Speeds PDF Author: C. C. Horstman
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 36

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The Flow about the Leading Edge of a Swept Blunt Plate at Hypersonic Speeds

The Flow about the Leading Edge of a Swept Blunt Plate at Hypersonic Speeds PDF Author: C. C. Horstman
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 36

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Book Description

The Flow about the Leading Edge of a Swept Blunt Plate at Hypersonic Speeds

The Flow about the Leading Edge of a Swept Blunt Plate at Hypersonic Speeds PDF Author: C. C. Horstman
Publisher:
ISBN:
Category :
Languages : en
Pages : 0

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Pressures on the Blunt Plate Wing at Supersonic and Hypersonic Speeds

Pressures on the Blunt Plate Wing at Supersonic and Hypersonic Speeds PDF Author: John D. Lee
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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).

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NASA Technical Note PDF Author:
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ISBN:
Category :
Languages : en
Pages : 488

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Scientific and Technical Aerospace Reports PDF Author:
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Category : Aerodynamics, Hypersonic
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