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AN INVESTIGATION AT SUBSONIC SPEEDS OF AERODYNAMIC CHARACTERISTICS AT ANGLES OF ATTACK FROM -4 DEG TO 100 DEG OF A DELTA-WING REENTRY CONFIGURATION HAVING FOLDING WINGTIP PANELS

Bernard Spencer

Published: 1960

Total Pages: 32

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An Investigation at Subsonic Speeds of Aerodynamic Characteristics at Angles of Attack from -4 to 100 of a Delta Wing Reentry Configuration Having Folding Wingtip Panels

Bernard Jr Spenser

Published: 1960

Total Pages: 28

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An Investigation at Subsonic Speeds of Aerodynamic Charactersitcs at Angles of Attack from -40 to 1000 of a Delta-wing Reentry Configuration Having Folding Wingtip Panels

Bernard Spencer

Published: 1960

Total Pages: 34

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An Investigation at Subsonic Speeds of the Longitudinal Aerodynamic Characteristics at Angles of Attach from -4° to 100° of Delta-wing Reentry Configurations Having Vertically Displaced and Cambered Wing-tip Panels

Bernard Spencer

Published: 1961

Total Pages: 38

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Subsonic aerodynamic characteristics of delta-wing reentry vehicle with vertically displaced and cambered wing-tip panels.

An Investigation at Subsonic Speeds of the Longitudinal Aerodynamic Characteristics at Angles of Attach from -4° to 100° of Delta-wing Reentry Configurations Having Vertically Displaced and Cambered Wing-tip Panels

Bernard Spencer

Published: 1961

Total Pages: 40

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Subsonic aerodynamic characteristics of delta-wing reentry vehicle with vertically displaced and cambered wing-tip panels.

High-subsonic-speed Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Delta-wing Configurations for Angles of Attack from 0° to 90°

Bernard Spencer

Published: 1959

Total Pages: 34

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Keywords Index to U.S. Government Technical Reports

Published: 1963-06-15

Total Pages: 88

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Keywords Index to U.S. Government Technical Reports (permuted Title Index).

United States. Department of Commerce. Office of Technical Services

Published: 1963

Total Pages: 618

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A Wind-tunnel Investigation of the Aerodynamic Characteristics of a Generalized Series of Winged Reentry Configurations at Angles of Attack to 180 Deg at Mach Numbers of 2.38, 2.99, and 4.00

Published: 1961

Total Pages: 72

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Static Longitudinal Aerodynamic Characteristics at Transonic Speeds and Angles of Attack Up to 99° of a Reentry Glider Having Folding Wing-tip Panels

Walter B. Olstad

Published: 1961

Total Pages: 36

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AN INVESTIGATION AT SUBSONIC SPEEDS OF AERODYNAMIC CHARACTERISTICS AT ANGLES OF ATTACK FROM -4 DEG TO 100 DEG OF A DELTA-WING REENTRY CONFIGURATION HAVING FOLDING WINGTIP PANELS

An Investigation at Subsonic Speeds of Aerodynamic Characteristics at Angles of Attack from -4 to 100 of a Delta Wing Reentry Configuration Having Folding Wingtip Panels

An Investigation at Subsonic Speeds of Aerodynamic Charactersitcs at Angles of Attack from -40 to 1000 of a Delta-wing Reentry Configuration Having Folding Wingtip Panels

An Investigation at Subsonic Speeds of the Longitudinal Aerodynamic Characteristics at Angles of Attach from -4° to 100° of Delta-wing Reentry Configurations Having Vertically Displaced and Cambered Wing-tip Panels

An Investigation at Subsonic Speeds of the Longitudinal Aerodynamic Characteristics at Angles of Attach from -4° to 100° of Delta-wing Reentry Configurations Having Vertically Displaced and Cambered Wing-tip Panels

High-subsonic-speed Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Delta-wing Configurations for Angles of Attack from 0° to 90°

Keywords Index to U.S. Government Technical Reports

Keywords Index to U.S. Government Technical Reports (permuted Title Index).

A Wind-tunnel Investigation of the Aerodynamic Characteristics of a Generalized Series of Winged Reentry Configurations at Angles of Attack to 180 Deg at Mach Numbers of 2.38, 2.99, and 4.00

Static Longitudinal Aerodynamic Characteristics at Transonic Speeds and Angles of Attack Up to 99° of a Reentry Glider Having Folding Wing-tip Panels

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