Numerical Simulation Of Hypersonic Flow Over A Blunt Leading Edge Delta Wing

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Numerical Simulation of Hypersonic Flow Over a Blunt Leading Edge Delta Wing

Numerical Simulation of Hypersonic Flow Over a Blunt Leading Edge Delta Wing
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Total Pages : 138
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ISBN-10 : OCLC:21570830
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Book Synopsis Numerical Simulation of Hypersonic Flow Over a Blunt Leading Edge Delta Wing by : Kuok-Ming Lee

Download or read book Numerical Simulation of Hypersonic Flow Over a Blunt Leading Edge Delta Wing written by Kuok-Ming Lee and published by . This book was released on 1989 with total page 138 pages. Available in PDF, EPUB and Kindle. Book excerpt:


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Numerical Simulation of Hypersonic Flow Over a Blunt Leading Edge Delta Wing
Language: en
Pages: 138
Authors: Kuok-Ming Lee
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On the Hypersonic Flow Past Blunted, Flat Delta Wings
Language: en
Pages: 48
Authors: Arnold Polak
Categories: Aerodynamics, Hypersonic
Type: BOOK - Published: 1970 - Publisher:

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The flow of a perfect gas over the slab portion of a blunted delta wing flying at hypersonic speeds is studied. A set of approximate equations is derived and a
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Language: en
Pages: 82
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Type: BOOK - Published: 1967 - Publisher:

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The object of the present analysis is to investigate the high-speed aerodynamic properties of a blunt delta wing at low angles of attack where the maximum lift
Numerical Simulation of the Flow Field Over Delta Wings with Leading Edge Blowing
Language: en
Pages: 228
Authors: David T. Yeh
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Type: BOOK - Published: 1988 - Publisher:

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Separated and Vortical Flow in Aircraft Wing Aerodynamics
Language: en
Pages: 458
Authors: Ernst Heinrich Hirschel
Categories: Technology & Engineering
Type: BOOK - Published: 2020-10-04 - Publisher: Springer Nature

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Fluid mechanical aspects of separated and vortical flow in aircraft wing aerodynamics are treated. The focus is on two wing classes: (1) large aspect-ratio wing