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Supersonic aerodynamic interference effects of store separation. Part 1: Computational analysis of cavity flowfieldsAn explicit-implicit and an implicit two-dimensional Navier-Stokes code along with various grid generation capabilities were developed. A series of classical benckmark cases were simulated using these codes.
Document ID
19870017424
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Baysal, Oktay (Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-180311
NAS 1.26:180311
Report Number: NASA-CR-180311
Report Number: NAS 1.26:180311
Accession Number
87N26857
Funding Number(s)
CONTRACT_GRANT: NAG1-559
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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