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 DEG TO 100 DEG OF A DELTA-WING REENTRY CONFIGURATION HAVING FOLDING WINGTIP PANELS PDF Author: Bernard Spencer
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ISBN:
Category : Air flow
Languages : en
Pages : 32

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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

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 PDF Author: Bernard Spencer
Publisher:
ISBN:
Category : Air flow
Languages : en
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

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 PDF Author: Bernard Spencer
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 40

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

Keywords Index to U.S. Government Technical Reports

Keywords Index to U.S. Government Technical Reports PDF Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 88

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

Keywords Index to U.S. Government Technical Reports (permuted Title Index). PDF Author: United States. Department of Commerce. Office of Technical Services
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Category : Government publications
Languages : en
Pages : 618

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Low Speed Aerodynamic Characteristics of a Modified Blunt 13 Deg Half-cone Lifting-body Configuration Having Deployable Horizontal Tails with Or Without Variable-sweep Wings

Low Speed Aerodynamic Characteristics of a Modified Blunt 13 Deg Half-cone Lifting-body Configuration Having Deployable Horizontal Tails with Or Without Variable-sweep Wings PDF Author:
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ISBN:
Category :
Languages : en
Pages : 52

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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

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 PDF Author:
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Category :
Languages : en
Pages : 72

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EFFECT OF LONGITUDINAL AND LATERAL CONTROLS ON AERODYNAMIC CHARACTERISTICS OF A WINGED REENTRY CONFIGURATION AT A MACH NUMBER OF 1.97 AND ANGLES OF ATTACK UP TO APPROXIMATELY 90 DEG

EFFECT OF LONGITUDINAL AND LATERAL CONTROLS ON AERODYNAMIC CHARACTERISTICS OF A WINGED REENTRY CONFIGURATION AT A MACH NUMBER OF 1.97 AND ANGLES OF ATTACK UP TO APPROXIMATELY 90 DEG PDF Author:
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Category :
Languages : en
Pages : 16

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

High-subsonic-speed Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Delta-wing Configurations for Angles of Attack from 0° to 90° PDF Author: Bernard Spencer
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 34

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Innovation in Flight

Innovation in Flight PDF Author: Joseph R. Chambers
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ISBN:
Category : Aeronautics
Languages : en
Pages : 406

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