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 Download

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

Book Description

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
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 32

Book Description

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

Book Description

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

Book Description
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:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 88

Book Description

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
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 618

Book Description

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 984

Book Description

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:
Publisher:
ISBN:
Category :
Languages : en
Pages : 72

Book Description

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

Static Longitudinal Aerodynamic Characteristics at Transonic Speeds and Angles of Attack Up to 99° of a Reentry Glider Having Folding Wing-tip Panels PDF Author: Walter B. Olstad
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 36

Book Description

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:
Publisher:
ISBN:
Category :
Languages : en
Pages : 52

Book Description

A Simplified Method for Estimating Subsonic Lift-curve Slope at Low Angles of Attack for Irregular Planform Wings

A Simplified Method for Estimating Subsonic Lift-curve Slope at Low Angles of Attack for Irregular Planform Wings PDF Author: Bernard Jr Spencer
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

Book Description

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