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.
General
Imprint: |
Bibliogov
|
Country of origin: |
United States |
Release date: |
July 2013 |
First published: |
July 2013 |
Authors: |
Jerry M. Allen
|
Dimensions: |
246 x 189 x 6mm (L x W x T) |
Format: |
Paperback - Trade
|
Pages: |
118 |
ISBN-13: |
978-1-287-25758-5 |
Categories: |
Books >
Social sciences >
Politics & government >
General
|
LSN: |
1-287-25758-5 |
Barcode: |
9781287257585 |
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