Longitudinal Aerodynamic Characteristics at Mach 1.50 to 4.63 of a Missile Model Employing Various Canards and a Trailing Edge Flap Control PDF Download

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Longitudinal Aerodynamic Characteristics at Mach 1.50 to 4.63 of a Missile Model Employing Various Canards and a Trailing Edge Flap Control

Longitudinal Aerodynamic Characteristics at Mach 1.50 to 4.63 of a Missile Model Employing Various Canards and a Trailing Edge Flap Control PDF Author: Charles D. Jr Trescot
Publisher:
ISBN:
Category :
Languages : en
Pages : 124

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Book Description

Longitudinal Aerodynamic Characteristics at Mach 1.50 to 4.63 of a Missile Model Employing Various Canards and a Trailing Edge Flap Control

Longitudinal Aerodynamic Characteristics at Mach 1.50 to 4.63 of a Missile Model Employing Various Canards and a Trailing Edge Flap Control PDF Author: Charles D. Jr Trescot
Publisher:
ISBN:
Category :
Languages : en
Pages : 124

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Book Description

Aerodynamic Characteristics at Mach Numbers from 1.50 to 4.63 of a Maneuverable Missile with In-line Cruciform Wings and Canard Surfaces

Aerodynamic Characteristics at Mach Numbers from 1.50 to 4.63 of a Maneuverable Missile with In-line Cruciform Wings and Canard Surfaces PDF Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 52

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Book Description
An investigation has been conducted in the Langley Unitary Plan wind tunnel at Mach numbers from 1.50 to 4.63 to determine the aerodynamic characteristics of a maneuverable missile having in-line cruciform wings and canard surfaces oriented in 45° roll planes.

Aerodynamic Characteristics for Combined Angles of Attack and Sideslip of Low-aspect-ratio Cruciform-wing Missile Configuration Employing Various Canard and Trailing-edge Flap Controls at Mach Number of 2.01 [with List of References]

Aerodynamic Characteristics for Combined Angles of Attack and Sideslip of Low-aspect-ratio Cruciform-wing Missile Configuration Employing Various Canard and Trailing-edge Flap Controls at Mach Number of 2.01 [with List of References] PDF Author: Ross B. Robinson
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 71

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Book Description

Longitudinal Aerodynamic Characteristics of a Fighter Model with a Close-coupled Canard at Mach Numbers from 0.40 to 1.20

Longitudinal Aerodynamic Characteristics of a Fighter Model with a Close-coupled Canard at Mach Numbers from 0.40 to 1.20 PDF Author: Richard J. Re
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 88

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Book Description

Longitudinal Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.86 for a Fixed-span Missile with Three Wing Planforms

Longitudinal Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.86 for a Fixed-span Missile with Three Wing Planforms PDF Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36

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Book Description

Longitudinal Aerodynamic Characteristics of a Fighter Model with a Close-coupled Canard at Mach Numbers from 0.40 to 1.20

Longitudinal Aerodynamic Characteristics of a Fighter Model with a Close-coupled Canard at Mach Numbers from 0.40 to 1.20 PDF Author: Richard J. Re
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 88

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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

Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.16 of a Blunt-nose Missile Model Having a Triangular Cross Section and Fixed Triform Fins

Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.16 of a Blunt-nose Missile Model Having a Triangular Cross Section and Fixed Triform Fins PDF Author: William J. Monta
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36

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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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Book Description

Longitudinal Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.86 for a Spanmissile with Three Wing Planforms

Longitudinal Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.86 for a Spanmissile with Three Wing Planforms PDF Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 34

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Book Description