Supersonic Stability and Control Characteristics of a Cruciform Missile Model with Delta Wings and Aft Tail Fin Control PDF Download

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Supersonic Stability and Control Characteristics of a Cruciform Missile Model with Delta Wings and Aft Tail Fin Control

Supersonic Stability and Control Characteristics of a Cruciform Missile Model with Delta Wings and Aft Tail Fin Control PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 124

Book Description


Supersonic Stability and Control Characteristics of a Cruciform Missile Model with Delta Wings and Aft Tail Fin Control

Supersonic Stability and Control Characteristics of a Cruciform Missile Model with Delta Wings and Aft Tail Fin Control PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 124

Book Description


Supersonic Stability and Control Characteristics of a Cruciform Missile Model with Delta Wings and Aft Tail Fin Controls

Supersonic Stability and Control Characteristics of a Cruciform Missile Model with Delta Wings and Aft Tail Fin Controls PDF Author: William A. Corlett
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 124

Book Description


Supersonic Stability and Control Characteristics of a Cruciform Missile Model with Delta Wings and Aft Tail Fin Controls

Supersonic Stability and Control Characteristics of a Cruciform Missile Model with Delta Wings and Aft Tail Fin Controls PDF Author: William A. Corlett
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 124

Book Description


NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 120

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1076

Book Description


Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 232

Book Description


A Study of Panel Loads and Centers of Pressure of Three Different Cruciform Aft-tail Control Surfaces of a Wingless Missile from Mach 1.60 to 3.70

A Study of Panel Loads and Centers of Pressure of Three Different Cruciform Aft-tail Control Surfaces of a Wingless Missile from Mach 1.60 to 3.70 PDF Author: Milton Lamb
Publisher:
ISBN:
Category :
Languages : en
Pages : 116

Book Description


Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1388

Book Description


R & D Abstracts

R & D Abstracts PDF Author: Technology Reports Centre (Great Britain)
Publisher:
ISBN:
Category :
Languages : en
Pages : 620

Book Description


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.