Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Book Description
An Aerodynamic Assessment of Various Missile Configuration Concepts
Author: Scientific and Technical Aerospace Reports
Author: Analysis and compilation of missile aerodynamic data
Author: James O. NicholsPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 326
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.
NASA Technical Memorandum
Author: Analysis and Compilation of Missile Aerodynamic Data. Volume 2: Performance Analysis
Author: John E. BurkhalterMissile 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.
Scientific and Technical Information Output of the Langley Research Center
Author: Technical Abstract Bulletin
Author: Monthly Catalog of United States Government Publications
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1130
Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index
Missile Aerodynamics
Author: Jack Norman NielsenPublisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN: 9780962062902
Category : Guided missiles
Languages : en
Pages : 450
Book Description
The similarities between the airplane and the missile extend beyond their flying capabilities, and at higher operational speeds, the configuration distinctions become even less apparent. " Missile Aerodynamics," a classic now available from AIAA and Nielsen Engineering and Research, Inc., combines the best of missile and airplane aerodynamics, drawing extensively from numerous technical papers to present a rational and unified account of the principles behind missile projection. Evaluate the missile versus the airplane in a multitude of areas, from longitudinal acceleration, wing loading, roll and dynamic stability, guidance and navigation, and more. J.N. Nielsen covers every aspect of missile aerodynamics, from the classification of missiles and basic formulas to innovative aerodynamic controls. In one reliable reference, readers will find hundreds of schematics, equations, and tables with practical applications in missile design and engineering. Originally published by Nielsen Engineering and Research, Inc.