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

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 Stability and Control Characteristics from a Flight Investigation of a Cruciform Canard Missile Configuration Having an Exposed Wing-canard Area Ratio of 16:1

Longitudinal Stability and Control Characteristics from a Flight Investigation of a Cruciform Canard Missile Configuration Having an Exposed Wing-canard Area Ratio of 16:1 PDF Author: Martin T. Moul
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 42

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

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

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 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 :
Languages : en
Pages : 1

Book Description
The investigation was conducted in the Langley 4- by 4-foot supersonic pressure tunnel. The missiles had cruciform wings and canard surfaces of delta planform with 70 degrees swept leading edges. Five models were tested with fineness ratios varying from 19.1 to 14.8. The tests covered an angle-of-attack range up to about 28 degrees for the complete configuration and various combinations of component parts. (Author).

Analysis and Compilation of Missile Aerodynamic Data: Data presentation and analysis

Analysis and Compilation of Missile Aerodynamic Data: Data presentation and analysis PDF Author: James O. Nichols
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 132

Book Description
This summary document was prepared in order to facilitate dissemination of a large amount of missile aerodynamic data which has recently been declassified. Only summary data are presented in this report, but a list of reference documents provides sources of detailed data. Most of the configurations considered are suitable for highly maneuverable air-to-air or surface to air missiles; however, data for a few air-to-surface, cruise missile, and one projectile configuration are also presented. The Mach number range of the data is from about 0.2 to 4.63; however, data for most configurations cover only a portion of this range. The following aerodynamic characteristics at various Mach numbers and zero angle of attack are presented.
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