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A zonal CFD method for three-dimensional wing simulationsThe primary objective of this work is to demonstrate the feasibility of a 3D potential/viscous flow coupling procedure for reducing computational effort while maintaining solution accuracy. The closed-loop, overlapped, velocity-coupling concept has been developed in a new code, ZAP3D, that couples a potential flow panel code with a Navier-Stokes method. The current ZAP3D calculation for an aspect ratio 5 wing with an outer domain radius of about 1.2 chords represents a speed-up in CPU time over the ARC3D large domain calculation by about a factor of 2.5. This improvement is achieved for less than a 0.5 percent deviation in C(L), 10 counts change in C(D), and 0.0015 variation in C(My). Additional reductions in the required computational domain for ZAP3D are expected as the method is further developed and refined.
Document ID
19930063228
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Summa, J. M.
(NASA Ames Research Center Moffett Field, CA, United States)
Strash, D. J.
(NASA Ames Research Center Moffett Field, CA, United States)
Yoo, S.
(Analytical Methods, Inc. Redmond, WA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: AIAA Applied Aerodynamics Conference, 11th, Monterey, CA, Aug. 9-11, 1993, Technical Papers. Pt. 1 (A93-47201 19-02)
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 93-3433
Accession Number
93A47225
Funding Number(s)
CONTRACT_GRANT: NAS2-13194
CONTRACT_GRANT: NAS2-12961
Distribution Limits
Public
Copyright
Other

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