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Virtual zone Navier-Stokes computations for oscillating control surfacesA new zoning method called 'virtual zones' has been developed for application to an unsteady finite difference Navier-Stokes code. The virtual zoning method simplifies the zoning and gridding of complex configurations for use with patched multi-zone flow codes. An existing interpolation method has been extensively modified to bring the run time for the interpolation procedure down to the same level as for the flow solver. Unsteady Navier-Stokes computations have been performed for transonic flow over a clipped delta wing with an oscillating control surface. The computed unsteady pressure and response characteristics of the control-surface motion compare well with experimental data.
Document ID
19930061059
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Klopfer, G. H.
(NASA Ames Research Center Moffett Field, CA, United States)
Obayashi, S.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: AIAA Computational Fluid Dynamics Conference, 11th, Orlando, FL, July 6-9, 1993, Technical Papers. Pt. 2 (A93-44994 18-34)
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 93-3363
Report Number: AIAA PAPER 93-3363
Accession Number
93A45056
Funding Number(s)
CONTRACT_GRANT: NCC2-605
CONTRACT_GRANT: NCC2-616
Distribution Limits
Public
Copyright
Other

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