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Global flowfield about the V-22 Tiltrotor AircraftThe Chimera overset grid method is reviewed and discussed in the context of a method of solution and analysis of unsteady three-dimensional viscous flows. The state of maturity of the various pieces of support software required to use the approach is discussed. A variety of recent applications of the method is presented. Current limitations of the approach are identified.
Document ID
19950020828
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Meakin, Robert L.
(Overset Methods, Inc. Los Altos, CA, United States)
Date Acquired
September 6, 2013
Publication Date
March 23, 1995
Subject Category
Aerodynamics
Report/Patent Number
OMI-01-92
NAS 1.26:198603
NASA-CR-198603
Accession Number
95N27248
Funding Number(s)
CONTRACT_GRANT: NCC2-747
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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