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Aerodynamics of Sounding-Rocket GeometriesTheoretical aerodynamics program TAD predicts aerodynamic characteristics of vehicles with sounding-rocket configurations. These slender, Axisymmetric finned vehicles have a wide range of aeronautical applications from rockets to high-speed armament. TAD calculates characteristics of separate portions of vehicle, calculates interference between portions, and combines results to form total vehicle solution.
Document ID
19810000074
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Barrowman, J.
Date Acquired
August 11, 2013
Publication Date
September 1, 1982
Publication Information
Publication: NASA Tech Briefs
Volume: 6
Issue: 1
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
GSC-12680
Accession Number
81B10074
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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