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Author : Roger S. Gates,G. L. Winchenback,John R. Cipolla,Mark A. Fische
Publisher : Unknown
Page : 14 pages
File Size : 47,7 Mb
Release : 1989
Category : Aerodynamics, Supersonic
ISBN : UOM:39015104957819
Author : G. L. Winchenbach
Publisher : Unknown
Page : 172 pages
File Size : 54,5 Mb
Release : 1997
Category : Aerodynamics
ISBN : UOM:39015104956365
Author : Anonim
Publisher : Unknown
Page : 766 pages
File Size : 46,5 Mb
Release : 1987-05
Category : Science
ISBN : CORNELL:31924057177242
Author : Anonim
Publisher : Unknown
Page : 702 pages
File Size : 49,8 Mb
Release : 1995
Category : Aeronautics
ISBN : UIUC:30112048646605
Author : Anonim
Publisher : Unknown
Page : 564 pages
File Size : 54,9 Mb
Release : 1991
Category : Aerodynamics
ISBN : PSU:000022141514
Author : American Institute of Aeronautics and Astronautics. Technical Information Service
Publisher : Unknown
Page : 226 pages
File Size : 51,8 Mb
Release : 1994
Category : AIAA paper
ISBN : UOM:39015030235983
Author : Anonim
Publisher : Unknown
Page : 974 pages
File Size : 51,9 Mb
Release : 1999
Category : Aeronautics
ISBN : STANFORD:36105021811372
Author : Anonim
Publisher : Unknown
Page : 638 pages
File Size : 44,7 Mb
Release : 1997
Category : Aeronautics
ISBN : STANFORD:36105021091975
Author : Anonim
Publisher : Unknown
Page : 356 pages
File Size : 50,6 Mb
Release : 1974
Category : Aerodynamics
ISBN : PSU:000017295017
Author : Anonim
Publisher : Unknown
Page : 340 pages
File Size : 40,6 Mb
Release : 1994
Category : Flight simulators
ISBN : PSU:000022713254
Author : Anonim
Publisher : Unknown
Page : 598 pages
File Size : 54,5 Mb
Release : 1992
Category : Aerodynamics
ISBN : PSU:000021943553
Author : Anonim
Publisher : Unknown
Page : 1120 pages
File Size : 48,8 Mb
Release : 1990
Category : Government reports announcements & index
ISBN : WISC:89049504491
Author : S. S. Chin
Publisher : Unknown
Page : 304 pages
File Size : 50,5 Mb
Release : 1961
Category : Guided missiles
ISBN : UOM:39015015426904
Beskriver principperne i f.m. konstruktionen af styrede missiler.
Author : N. Uchiyama,Jain-Ming Wu
Publisher : Unknown
Page : 190 pages
File Size : 51,6 Mb
Release : 1976
Category : Aerodynamic load
ISBN : UOM:39015095343235
The aerodynamic loading on a number of rocket body-control surface combinations has been calculated using methods developed at the University of Tennessee Space Institute over the past five years. Variations in control surface planform, roll angle, control surface deflection or incorporation of elevons, are included. Compressibility is accounted for. Details of the digital computer program are included.
Author : James O. Nichols
Publisher : Unknown
Page : 132 pages
File Size : 44,8 Mb
Release : 1977
Category : Aerodynamic load
ISBN : STANFORD:36105024664703
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.