Longitudinal Stability and Control Characteristics of a Winged and a Flared Hypersonic Missile Configuration with Various Nose Shapes and Flare Modifications at a Mach Number of 2.01 PDF Download

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Longitudinal Stability and Control Characteristics of a Winged and a Flared Hypersonic Missile Configuration with Various Nose Shapes and Flare Modifications at a Mach Number of 2.01

Longitudinal Stability and Control Characteristics of a Winged and a Flared Hypersonic Missile Configuration with Various Nose Shapes and Flare Modifications at a Mach Number of 2.01 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 32

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Book Description

Longitudinal Stability and Control Characteristics of a Winged and a Flared Hypersonic Missile Configuration with Various Nose Shapes and Flare Modifications at a Mach Number of 2.01

Longitudinal Stability and Control Characteristics of a Winged and a Flared Hypersonic Missile Configuration with Various Nose Shapes and Flare Modifications at a Mach Number of 2.01 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 32

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Book Description

Static Longitudinal Stability and Control Characteristics at a Mach Number of 2.01 of a Hypersonic Missile Configuration Having All-movable Wing and Tail Surfaces

Static Longitudinal Stability and Control Characteristics at a Mach Number of 2.01 of a Hypersonic Missile Configuration Having All-movable Wing and Tail Surfaces PDF Author: Ross B. Robinson
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 32

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Book Description

Longitudinal Stability and Control Characteristics at Mach Numbers of 2.01, 4.65, and 6.8 of Two Hypersonic Missile Configurations, One Having Low-aspect-ratio Cruciform Wings with Trailing-edge Flaps and One Having a Flared Afterbody and All-movable Cont

Longitudinal Stability and Control Characteristics at Mach Numbers of 2.01, 4.65, and 6.8 of Two Hypersonic Missile Configurations, One Having Low-aspect-ratio Cruciform Wings with Trailing-edge Flaps and One Having a Flared Afterbody and All-movable Cont PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

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Static Longitudinal Stability of a Missile Configuration with Various Nose Shapes and Flared Afterbodies at a Mach Number of 6.82

Static Longitudinal Stability of a Missile Configuration with Various Nose Shapes and Flared Afterbodies at a Mach Number of 6.82 PDF Author: Jim A. Penland
Publisher:
ISBN:
Category :
Languages : en
Pages : 102

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Book Description

Static Longitudinal Stability and Control Characteristics at a Mach Number of 2.01 of a Hypersonic Missile Configuration Having All-movable Wing and Tail Surfaces

Static Longitudinal Stability and Control Characteristics at a Mach Number of 2.01 of a Hypersonic Missile Configuration Having All-movable Wing and Tail Surfaces PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 32

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Book Description

Government-wide Index to Federal Research & Development Reports

Government-wide Index to Federal Research & Development Reports PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1654

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Book Description

An Experimental and Theoretical Study of the Aerodynamic Characteristics of Some Generic Missile Concepts at Mach Numbers from 2 to 6.8

An Experimental and Theoretical Study of the Aerodynamic Characteristics of Some Generic Missile Concepts at Mach Numbers from 2 to 6.8 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

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Book Description

Longitudinal Stability and Control Characteristics at Mach Numbers of 2.01, 4.65, and 6.8 of Two Hypersonic Missile Configurations, One Having Low-aspect-ratio Cruciform Wings with Trailing Edge Flaps and One Having a Flared Afterbody and All Movable Controls

Longitudinal Stability and Control Characteristics at Mach Numbers of 2.01, 4.65, and 6.8 of Two Hypersonic Missile Configurations, One Having Low-aspect-ratio Cruciform Wings with Trailing Edge Flaps and One Having a Flared Afterbody and All Movable Controls PDF Author: Leroy M. Spearman
Publisher:
ISBN:
Category :
Languages : en
Pages : 30

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Book Description

Sideslip Characteristics at Various Angles of Attack for Several Hypersonic Missile Configurations with Canard Controls at a Mach Number of 2.01

Sideslip Characteristics at Various Angles of Attack for Several Hypersonic Missile Configurations with Canard Controls at a Mach Number of 2.01 PDF Author: Gerald V. Foster
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 30

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Book Description

Longitudinal Stability and Control Characteristics of a Generalized Missile Configuration Employing Several Different Bulk Type Control Schemes at a Mach Number of 6.01

Longitudinal Stability and Control Characteristics of a Generalized Missile Configuration Employing Several Different Bulk Type Control Schemes at a Mach Number of 6.01 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 84

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Book Description