Aerodynamic Characteristics of 0.187-scale Model of a Target Missile at Mach 1.80 to 2.16
Author : William A. Corlett
Publisher :
Page : 84 pages
File Size : 40,96 MB
Release : 1966
Category :
ISBN :
Author : William A. Corlett
Publisher :
Page : 84 pages
File Size : 40,96 MB
Release : 1966
Category :
ISBN :
Author : J. H. Jones
Publisher :
Page : 220 pages
File Size : 26,97 MB
Release : 1972
Category : Drag (Aerodynamics)
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Static-force tests were conducted at Mach number 2.25, 3, and 4 on a 0.25 -scale model of the Beech High Altitude Supersonic Target (HAST) missile.
Author : William J. Monta
Publisher :
Page : 36 pages
File Size : 26,16 MB
Release : 1971
Category : Aerodynamics
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Author : William F. Hinson
Publisher :
Page : 52 pages
File Size : 48,75 MB
Release : 1969
Category : Pitching (Aerodynamics)
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Aerodynamic characteristics in pitch of scale model of two and three stage rocket configuration at Mach numbers of 0.4 to 4.63.
Author : Edward F. Ulmann
Publisher :
Page : 34 pages
File Size : 47,76 MB
Release : 1954
Category : Ballistic missiles
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Tests were conducted at Mach number 4.05 to determine the aerodynamic characteristics of several missile models having turbulent boundary layers and to compare these results with available method of predicting the aerodynamic characteristics. (The condition of the boundary layer was determined by the china-clay-lacquer boundary-layer-visualization technique.) Normal force and pitching moment were measured through an angle-of-attack range of 0 to between 4 and 8 degrees, depending upon balance limitations, and at roll angles of 0 and 45 degrees; drag was measured only at 0 degrees angle of attack.
Author : J. H. Jones
Publisher :
Page : 0 pages
File Size : 34,66 MB
Release : 1972
Category : Drag (Aerodynamics).
ISBN :
Static-force tests were conducted at Mach number 2.25, 3, and 4 on a 0.25 -scale model of the Beech High Altitude Supersonic Target (HAST) missile.
Author : M. Leroy Spearman
Publisher :
Page : 36 pages
File Size : 14,44 MB
Release : 1977
Category : Aerodynamics
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Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 936 pages
File Size : 12,34 MB
Release : 1963
Category : Aeronautics
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Author : J. T. Best (Jr.)
Publisher :
Page : 194 pages
File Size : 29,7 MB
Release : 1974
Category : Drag (Aerodynamics)
ISBN :
Static-force tests were conducted at Mach number 2.25, 3, and 4 on a 0.25 -scale model of the High Altitude Supersonic Target (HAST) missile.
Author : Ross B. Robinson
Publisher :
Page : 42 pages
File Size : 48,79 MB
Release : 1961
Category : Aerodynamics
ISBN :