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Loads and Pressures on Axisymmetric Bodies with Cruciform FinsNSWCDM computer program calculates aerodynamic loading and pressure distributions on supersonic configurations consisting of axisymmetric bodies with cruciform or planar canard and tail fins. Versatile program allows for configuration pitched and rolled, and fins deflected. Tail fins are interdigitated with respect to forward fins.
Document ID
19820000311
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Dillenius, M. F. E. (Nielsen Engineering & Research, Inc.)
Smith, C. A. (Nielsen Engineering & Research, Inc.)
Date Acquired
August 10, 2013
Publication Date
May 1, 1983
Publication Information
Publication: NASA Tech Briefs
Volume: 7
Issue: 2
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-12936
Accession Number
82B10311
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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