Exploratory Investigation at Mach Number of 2.01 of the Longitudinal Stability and Control Characteristics of a Winged Reentry Configuration

Exploratory Investigation at Mach Number of 2.01 of the Longitudinal Stability and Control Characteristics of a Winged Reentry Configuration PDF Author: Gerald V. Foster
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 28

Book Description

Exploratory Investigation at Mach Number of 2.01 of Longitudinal Stability and Control Characteristics of Winged Reentry Configuration [with List of References]

Exploratory Investigation at Mach Number of 2.01 of Longitudinal Stability and Control Characteristics of Winged Reentry Configuration [with List of References] PDF Author:
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 21

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.

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

Summary of Aerodynamic Characteristics of a Winged Reentry Vehicle at Mach Numbers from 0.06 to 9.6 with Detailed Results at a Mach Number of 9.6

Summary of Aerodynamic Characteristics of a Winged Reentry Vehicle at Mach Numbers from 0.06 to 9.6 with Detailed Results at a Mach Number of 9.6 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 68

Book Description

Static Stability and Control Characteristics of a Proposed Winged Reentry Vehicle at Mach Numbers of 1.50, 2.96, and 4.63

Static Stability and Control Characteristics of a Proposed Winged Reentry Vehicle at Mach Numbers of 1.50, 2.96, and 4.63 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 78

Book Description

Low-subsonic-speed Static Longitudinal Stability and Control Characteristics of a Winged Reentry-vehicle Configuration Having Wingtip Panels that Fold Up for High-drag Reentry

Low-subsonic-speed Static Longitudinal Stability and Control Characteristics of a Winged Reentry-vehicle Configuration Having Wingtip Panels that Fold Up for High-drag Reentry PDF Author: George M. Ware
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 20

Book Description

Effect of Longitudinal and Lateral Controls on Winged Reentry Configuration at Mach 1.97 and Angles of Attack Up to 90°

Effect of Longitudinal and Lateral Controls on Winged Reentry Configuration at Mach 1.97 and Angles of Attack Up to 90° PDF Author: Gerald V. Foster
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 20

Book Description

Static Longitudinal and Lateral Stability Characteristics at a Mach Number of 3.11 of Square and Circular Plan-form Reentry Vehicles, with Some Effects of Controls and Leading-edge Extensions

Static Longitudinal and Lateral Stability Characteristics at a Mach Number of 3.11 of Square and Circular Plan-form Reentry Vehicles, with Some Effects of Controls and Leading-edge Extensions PDF Author: Byron M. Jaquet
Publisher:
ISBN:
Category : Leading edges (Aerodynamics)
Languages : en
Pages : 26

Book Description

➤