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Author : Anonim
Publisher : Unknown
Page : 40 pages
File Size : 50,6 Mb
Release : 1991
Category : Guided missiles
ISBN : MINN:31951D031473186
Author : Anonim
Publisher : Unknown
Page : 0 pages
File Size : 46,8 Mb
Release : 1991
Category : Guided missiles
ISBN : OCLC:682668768
Author : Anonim
Publisher : Unknown
Page : 40 pages
File Size : 52,9 Mb
Release : 1991
Category : Guided missiles
ISBN : IND:30000097836682
Author : George Y. Jumper (Jr.),C. J. Frushon,R. K. Longstreth,J. Smith,J. Willett,D. Curtis
Publisher : Unknown
Page : 40 pages
File Size : 48,9 Mb
Release : 1991
Category : Guided missiles
ISBN : UOM:39015095311745
Author : Anonim
Publisher : Unknown
Page : 356 pages
File Size : 50,5 Mb
Release : 1974
Category : Aerodynamics
ISBN : PSU:000017295017
Author : Frank J. Regan
Publisher : Unknown
Page : 116 pages
File Size : 41,9 Mb
Release : 1970
Category : Aerodynamics, Supersonic
ISBN : UOM:39015095150697
A research configuration was formed by attaching wraparound fins in a cruciform arrangement to a 10-caliber Army-Navy spinner projectile. This configuration was tested in a supersonic tunnel to get the Magnus force and moment, as well as the normal force and pitching moment. Model spin rate was generated by means of fin cant.
Author : Anonim
Publisher : Unknown
Page : 1460 pages
File Size : 47,7 Mb
Release : 1991
Category : Aeronautics
ISBN : UIUC:30112001077426
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author : Anonim
Publisher : Unknown
Page : 636 pages
File Size : 53,8 Mb
Release : 1973
Category : Mechanics, Applied
ISBN : UCAL:C2682443
Author : United States. Superintendent of Documents
Publisher : Unknown
Page : 1300 pages
File Size : 44,8 Mb
Release : 1978
Category : United States
ISBN : STANFORD:36105022657543
Author : Frank J. Regan,J. H. Shannon,F. J. Tanner
Publisher : Unknown
Page : 64 pages
File Size : 48,8 Mb
Release : 1974
Category : Ballistics
ISBN : UOM:39015095246818
Since 1964 extensive and successful collaboration in a bomb dynamics program has continued between research organizations in Australia, the United Kingdom and the United States. Various aspects of this joint effort have been reported in separate reports: Part 1 treated the dynamics, aerodynamics and performance of free-fall weapons stabilized by fixed cruciform stabilizers. Part 2 gave a similar treatment of split-skirt stabilizers. Part 3 reviewed results obtained from the use of freely spinning panel stabilizers. This series of reports is concluded in the present document which discusses the task of the ballistician in light of the knowledge gained during the program and illustrates the application of the techniques derived to missile design. In addition, brief reference is made to a number of research projects which have stemmed from the original tripartite work.
Author : W. E. Scott
Publisher : Unknown
Page : 44 pages
File Size : 46,6 Mb
Release : 1960
Category : Rockets (Ordnance)
ISBN : UOM:39015095104769
Author : Anonim
Publisher : Unknown
Page : 662 pages
File Size : 54,7 Mb
Release : 1992
Category : Aeronautics
ISBN : STANFORD:36105001842579
Author : Anonim
Publisher : Unknown
Page : 726 pages
File Size : 54,8 Mb
Release : 1993
Category : Science
ISBN : MINN:31951P003205187
Author : Frank J. Regan
Publisher : Unknown
Page : 126 pages
File Size : 50,5 Mb
Release : 1972
Category : Body of revolution
ISBN : UOM:39015095152735
Base bleed is a technique whereby all or part of the boundary layer is 'bled' from the rear portion of a projectile to the base region. Passage from the model's surface to the base region is by means of concentric cylindrical passageways. The purpose of base bleed is to reduce the Magnus moment on overlong spinning bodies of revolution and to reduce the base drag. Both analytic and experimental results are presented. The boundary layer is represented by means of the momentum thickness.
Author : Anonim
Publisher : Unknown
Page : 1800 pages
File Size : 40,7 Mb
Release : 1993
Category : Government reports announcements & index
ISBN : MINN:30000003749342