Axial Forces on Cone-Cylinders in Transitional Rarefied Hypersonic Flow
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Page : 48 pages
File Size : 14,75 MB
Release : 1970
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Author :
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Page : 48 pages
File Size : 14,75 MB
Release : 1970
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Author : David E. Boylan
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Page : 41 pages
File Size : 17,3 MB
Release : 1970
Category : Aerodynamics, Hypersonic
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Axial forces were measured on cone-cylinder configurations under hypersonic, cold wall, rarefied flow conditions. Measurements were obtained in the angle-of-attack range 0
Author : T. J. Rhys-Jones
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Page : 12 pages
File Size : 36,24 MB
Release : 1987
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This Paper describes an experimental study performed in the RAE Low Density Tunnel to determine the aerodynamic characteristics of a range of slender axisymmetric bodies in rarefied hypersonic flow. The main purpose of this study was to assess the effects of cone angle, nose bluntness and Reynolds number on the zero incidence drag of cones. In addition, some measurements of axial force, normal force and pitching moment at incidence were made. The bodies were tested at a nominal Mach number of 10 and at flow conditions which correspond to those in the transitional rarefied flow regime. These data have been compared with correlations developed to represent the change in drag coefficient in this flow regime between continuum and free molecular flow.
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Page : 1134 pages
File Size : 27,72 MB
Release : 1989
Category : Aeronautics
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Author : Marvin I. Kussoy
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Page : 20 pages
File Size : 18,41 MB
Release : 1967
Category : Aerodynamics, Supersonic
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Author : Desikan Bharathan
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Page : 86 pages
File Size : 12,96 MB
Release : 1972
Category : Hypersonic wind tunnels
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Author : Theodore Conrad Nark
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Page : 98 pages
File Size : 10,98 MB
Release : 1958
Category : Aerodynamics, Supersonic
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Page : 25 pages
File Size : 36,36 MB
Release : 1971
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Author : Richard D. Wagner (Jr.)
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Page : 40 pages
File Size : 37,9 MB
Release : 1964
Category : Aerodynamics, Hypersonic
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Author : Marvin I. Kussoy
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Page : 6 pages
File Size : 16,46 MB
Release : 1969
Category : Aerodynamics, Hypersonic
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