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Aeroelastic Computations For Wings With Loaded TipsExternal fuel tanks or missiles degrade stability because of unsteady aerodynamics. Transonic aeroelasticity of wings with tip stores simulated with improved version of ATRAN3S computer code, previously used to study behavior of clean wings only. Output of code agrees well with wind-tunnel data.
Document ID
19880000251
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Goorjian, Peter M. (NASA Ames Research Center, Moffett Field, Calif.)
Tu, Eugene L. (NASA Ames Research Center, Moffett Field, Calif.)
Guruswamy, Guru P. (Sterling Software)
Date Acquired
August 13, 2013
Publication Date
April 1, 1988
Publication Information
Publication: NASA Tech Briefs
Volume: 12
Issue: 4
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-11753
Report Number: ARC-11753
ISSN: 0145-319X
Accession Number
88B10251
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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