Author :
Publisher :
Page : 46 pages
File Size : 16,30 MB
Release : 1964
Category :
ISBN :
Author : M. Leroy Spearman
Publisher :
Page : 44 pages
File Size : 18,1 MB
Release : 1961
Category : Aerodynamics
ISBN :
Author : M. Leroy Spearman
Publisher :
Page : 52 pages
File Size : 46,7 MB
Release : 1967
Category : Guided missiles
ISBN :
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.
Author :
Publisher :
Page : 40 pages
File Size : 27,86 MB
Release : 1983
Category :
ISBN :
Author :
Publisher :
Page : 16 pages
File Size : 32,63 MB
Release : 1983
Category :
ISBN :
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 116 pages
File Size : 24,91 MB
Release : 2018-06-15
Category :
ISBN : 9781721146192
An experimental study has been performed to develop a large force and moment aerodynamic data set on a slender axisymmetric missile configuration having cruciform strakes and in-line control tail fins. The data include six-component balance measurements of the configuration aerodynamics and three-component measurements on all four tail fins. The test variables include angle of attack, roll angle, Mach number, model buildup, strake length, nose size, and tail fin deflection angles to provide pitch, yaw, and roll control. Test Mach numbers ranged from 0.60 to 4.63. The entire data set is presented on a CD-ROM that is attached to this paper. The CD-ROM also includes extensive plots of both the six-component configuration data and the three-component tail fin data. Selected samples of these plots are presented in this paper to illustrate the features of the data and to investigate the effects of the test variables. Allen, Jerry M. Langley Research Center WU 23-090-20-35
Author : James O. Nichols
Publisher :
Page : 132 pages
File Size : 41,37 MB
Release : 1977
Category : Aerodynamic load
ISBN :
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 : M. Leroy Spearman
Publisher :
Page : 36 pages
File Size : 33,36 MB
Release : 1977
Category : Aerodynamics
ISBN :
Author : M. Leroy Spearman
Publisher :
Page : 34 pages
File Size : 44,55 MB
Release : 1977
Category : Aerodynamics
ISBN :
Author : James O. Nichols
Publisher :
Page : 132 pages
File Size : 35,67 MB
Release : 1977
Category : Aerodynamic load
ISBN :
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.
