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

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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

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 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

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 of a Maneuverable Missile with Cruiform Wings and In-line Canard Surfaces at Mach Numbers from 0.50 to 4.63

Aerodynamic Characteristics of a Maneuverable Missile with Cruiform Wings and In-line Canard Surfaces at Mach Numbers from 0.50 to 4.63 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 100

Book Description

Aerodynamic Characteristics in Pitch of a Series of Cruciform-wing Missiles with Canard Controls at a Mach Number of 2.01

Aerodynamic Characteristics in Pitch of a Series of Cruciform-wing Missiles with Canard Controls at a Mach Number of 2.01 PDF Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44

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

Book Description

An Aerodynamic Assessment of Various Missile Configuration Concepts

An Aerodynamic Assessment of Various Missile Configuration Concepts PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 40

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

Book Description

Supersonic Aerodynamic Characteristics of a Cruciform Missile Configuration with Low-a-spect-ratio Wings and In-line Tail Controls

Supersonic Aerodynamic Characteristics of a Cruciform Missile Configuration with Low-a-spect-ratio Wings and In-line Tail Controls PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 46

Book Description

Aerodynamic Characteristics of a Cruciform-wing Missile with Canard Control Surfaces and of Some Very Small Span Wing-body Missiles at a Mach Number of 1.41

Aerodynamic Characteristics of a Cruciform-wing Missile with Canard Control Surfaces and of Some Very Small Span Wing-body Missiles at a Mach Number of 1.41 PDF Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 27

Book Description

Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards

Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards PDF Author: A. Warner Robins
Publisher:
ISBN:
Category : Hypersonic planes
Languages : en
Pages : 68

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

Book Description

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