NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Aeroelastic, CFD, and Dynamic Computation and Optimization for Buffet and Flutter ApplicationThe work presented in this paper include: 'Coupled and Uncoupled Bending-Torsion Responses of Twin-Tail Buffet'; 'Fluid/Structure Twin Tail Buffet Response Over a Wide Range of Angles of Attack'; 'Resent Advances in Multidisciplinary Aeronautical Problems of Fluids/Structures/Dynamics Interaction'; and'Development of a Coupled Fluid/Structure Aeroelastic Solver with Applications to Vortex Breakdown induced Twin Tail Buffeting.
Document ID
19980008111
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Kandil, Osama A.
(Old Dominion Univ. Norfolk, VA United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1997
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.26:206678
NASA/CR-97-206678
ODURF-164069
Report Number: NAS 1.26:206678
Report Number: NASA/CR-97-206678
Report Number: ODURF-164069
Funding Number(s)
CONTRACT_GRANT: NAG1-648
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available