The Leading-edge Effects on a Laminar Flat-plane Boundary Layer at Mach 10.4 PDF Download
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Author: Howard W. Stone
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 206
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Author: Howard W. Stone
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 206
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Author: Howard W. Stone
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44
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Author: Marcus O. Creager
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 36
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Author: Don W. Jillie
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 36
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Author: Anthony W. Fiore
Publisher:
ISBN:
Category : Turbulent boundary layer
Languages : en
Pages : 962
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Book Description
In 1975 the U.S. Air Force and the Federal Republic of Germany signed a Data Exchange Agreement numbered AF-75-G-7440 entitled 'Viscous and Interacting Flow Fields.' The purpose was to exchange data in the area of boundary layer research. It includes both experimental and theoretical boundary layer research at speeds from subsonic to hypersonic Mach numbers in the presence of laminar, transitional, and turbulent boundary layers. The main effort in recent years has been on turbulent boundary layers, both attached and separated in the presence of such parameters as pressure gradients, wall temperature, surface roughness, etc. In the United States the research was conducted in various Department of Defense, NASA, aircraft corporations, and various university laboratories. In the Federal Republic of Germany it was carried out within the various DFVLR, industrial, and university research centers.
Author: Paul F. Holloway
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 52
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Author: Marcus O. Creager
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
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Author: John Benjamin Anders
Publisher:
ISBN:
Category : Boundary layer control
Languages : en
Pages : 36
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Author: Thorval Tendeland
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 64
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Author: Don W. Jillie
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
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