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Navier-Stokes dynamics and aeroelastic computations for vortical flows, buffet and aeroelastic applicationsThe accomplishments achieved during the period include conference and proceedings publications, journal papers, and abstracts which are either published, accepted for publication or under review. Conference presentations and NASA highlight publications are also included. Two of the conference proceedings publications are attached along with a Ph.D. dissertation abstract and table of contents. In the first publication, computational simulation of three-dimensional flows around a delta wing undergoing rock and roll-divergence motions is presented. In the second publication, the unsteady Euler equations and the Euler equations of rigid body motion, both written in the moving frame of reference, are sequetially solved to simulate the limit-cycle rock motion of slender delta wings. In the dissertation abstract, unsteady flows around rigid or flexible delta wings with and without oscillating leading-edge flaps are considered.
Document ID
19930000910
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kandil, Osama A.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1992
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:190692
NASA-CR-190692
Report Number: NAS 1.26:190692
Report Number: NASA-CR-190692
Accession Number
93N10098
Funding Number(s)
CONTRACT_GRANT: NAG1-648
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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