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Calculation Of Aeroelastic Transients Using Euler EquationsMethod for calculation of transient aeroelastic effects on airplane wings based on Euler equations of flow. Conforming grids facilitate calculations of flows about changing shapes. Capability to compute aeroelastic effects reduces cost of developing aircraft.
Document ID
19910000209
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Guruswamy, Guru P. (NASA Ames Research Center, Moffett Field, CA.)
Date Acquired
August 14, 2013
Publication Date
May 1, 1991
Publication Information
Publication: NASA Tech Briefs
Volume: 15
Issue: 5
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-12351
ISSN: 0145-319X
Report Number: ARC-12351
Accession Number
91B10209
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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