An Experimental Investigation of the Interaction Between a Shock Wave and a Turbulent Boundary Layer on a Convex Wall PDF Download
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Author: C. Nebbeling
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
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Author: C. Nebbeling
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
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Author: C. C. Sun
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ISBN:
Category : Shock waves
Languages : en
Pages : 916
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Book Description
Tabulated data from a series of experimental studies of the interaction of a shock wave with a turbulent boundary layer in axisymmetric flow configurations is presented. The studies were conducted at the walls of circular wind tunnels and on the cylindrical centerbody of an annular flow channel. Detailed pitot pressure profiles and wall static pressure profiles upstream of, within and downstream of the interaction region are given. Results are presented for flows at nominal freestream Mach Numbers of 2, 3 and 4. For studies at the tunnel sidewalls, the shock waves were produced by conical shock generators mounted on the centerline of the wind tunnel at zero angle of attack. The annular ring generator was used to produce the shock wave at the centerbody of the annular flow channel. The effects of boundary layer bleed were examined in the investigation. Both bleed rate and bleed location were studied. Most of the bleed studies were conducted with bleed holes drilled normal to the wall surface but the effects of slot suction were also examined. A summary of the principal results and conclusions is given.
Author:
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Category : Aeronautics
Languages : en
Pages : 428
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Author: Gary Clifford Teeter
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Category : Shock waves
Languages : en
Pages : 148
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Author: Chen-Chih Sun
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ISBN:
Category : Shock waves
Languages : en
Pages : 916
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Author:
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Category : Aeronautics
Languages : en
Pages : 892
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Author:
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ISBN:
Category :
Languages : en
Pages : 88
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Author: David William Kuntz
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Category :
Languages : en
Pages : 544
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Author: Earl C. Watson
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ISBN:
Category : Laminar boundary layer
Languages : en
Pages : 140
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Book Description
Laminar and turbulent boundary layer interactions with externally generated shock waves.
Author: Marie H. Tuttle
Publisher:
ISBN:
Category : Interference (Aerodynamics)
Languages : en
Pages : 96
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