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Unsteady hybrid vortex technique for transonic vortex flows and flutter application

Author
Kandil, Osama A.
Published
Aug 1, 1987.
Physical Description
1 electronic document
Online Version

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Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Papers resulting from work performed from January 1, 1987 to July 31, 1987 are listed. Transonic computational schemes based on Integral Equation Formulation of the full potential equation were presented. Classical and zero-total pressure-loss sets of Euler equations applied to delta wings were examined.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19870018190.
Accession ID: 87N27623.
NASA-CR-180308.
NAS 1.26:180308.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15697686