Mach 6 Flow Field Surveys Beneath the Forebody of an Airbreatinng Missile
Author : Patrick J. Johnston
Publisher :
Page : 160 pages
File Size : 11,46 MB
Release : 1986
Category : Aerodynamics, Hypersonic
ISBN :
Author : Patrick J. Johnston
Publisher :
Page : 160 pages
File Size : 11,46 MB
Release : 1986
Category : Aerodynamics, Hypersonic
ISBN :
Author : Patrick J. Johnston
Publisher :
Page : 160 pages
File Size : 17,17 MB
Release : 1986
Category : Aerodynamics, Hypersonic
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Author : Walter F. Lindsey
Publisher :
Page : 44 pages
File Size : 23,78 MB
Release : 1970
Category : Aerodynamics
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Author : Ronald D. Brown
Publisher :
Page : 40 pages
File Size : 16,90 MB
Release : 1963
Category : Ablative materials
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Author : Langley Research Center
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Page : 44 pages
File Size : 35,4 MB
Release : 1964
Category : Aeronautics
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Author : Kalman J. Grunwald
Publisher :
Page : 148 pages
File Size : 20,77 MB
Release : 1970
Category : Buffeting (Aerodynamics)
ISBN :
A series of force tests was conducted on unpowered, high-speed ground-vehicle model configurations to provide information on shapes of this type very near the ground. Of particular interest were the crosswind effects on the aerodynamic forces and moments of the six models tested. These tests were conducted over the moving-belt ground plane in the 17-foot (5.18-m) test section of the Langley 300-MPH 7-by 10-foot tunnel at free-stream dynamic pressure values of 10 lb/ft2 (478.8 N/m2). The results indicate that the half-circle configuration is desirable because of the low rolling moments it experienced; however, it did have higher lift values than the other configurations and, from a utility standpoint, could be impractical. The half-circle configurations with extended sides may make good compromise configurations. All the ground-simulation techniques employed -moving ground belt, fixed ground belt, and image model -gave reasonable representations of the overall aerodynamic trends.
Author : Lloyd S. Jernell
Publisher :
Page : 28 pages
File Size : 18,90 MB
Release : 1970
Category : Aerodynamic load
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Drag coefficients of oblate spheroid and sphere at Mach numbers from 1.70 to 10.49.
Author : James C. Patterson
Publisher :
Page : 84 pages
File Size : 10,47 MB
Release : 1966
Category :
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Author : W. Frank Staylor
Publisher :
Page : 48 pages
File Size : 29,46 MB
Release : 1964
Category : Aerodynamics, Transonic
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Author : Nancy Jane Cyrus
Publisher :
Page : 36 pages
File Size : 41,9 MB
Release : 1968
Category : Differential equations, Linear
ISBN :