Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Book Description
An Aerodynamic Assessment of Various Missile Configuration Concepts
Author: Aerodynamic Test and Analysis of a Slender Generic Missile Configuration
Author: Roger S. GatesPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 14
Book Description
Analysis and Compilation of Missile Aerodynamic Data: Data presentation and analysis
Author: James O. NicholsPublisher:
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.
Scientific and Technical Aerospace Reports
Author: Missile Configuration Design
Author: S. S. ChinPublisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 304
Book Description
Beskriver principperne i f.m. konstruktionen af styrede missiler.
Analysis and Compilation of Missile Aerodynamic Data. Volume 1: Data Presentation and Analysis
Author: James O. NicholsPublisher:
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.
Aerodynamic Configured Missile Development
Author: Robert J. KriegerPublisher:
ISBN:
Category : Cruise missiles
Languages : en
Pages : 136
Book Description
This report presents the results of a program that investigated aerodynamic configuring as a method of improving long range supersonic cruise and maneuvering missile performance. Non-circular body, lifting body, blended wing body, wing-body and favorable interference concepts were developed and wind tunnel tested. Substantial improvements in cruise range were shown to result from aero configuring.
Analysis and Compilation of Missile Aerodynamic Data
Author: James O. NicholsPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages :
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.
Author: 
Author: Clyde Hayes