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Automation of a N-S S and C Database Generation for the Harrier in Ground EffectA method of automating the generation of a time-dependent, Navier-Stokes static stability and control database for the Harrier aircraft in ground effect is outlined. Reusable, lightweight components arc described which allow different facets of the computational fluid dynamic simulation process to utilize a consistent interface to a remote database. These components also allow changes and customizations to easily be facilitated into the solution process to enhance performance, without relying upon third-party support. An analysis of the multi-level parallel solver OVERFLOW-MLP is presented, and the results indicate that it is feasible to utilize large numbers of processors (= 100) even with a grid system with relatively small number of cells (= 10(exp 6)). A more detailed discussion of the simulation process, as well as refined data for the scaling of the OVERFLOW-MLP flow solver will be included in the full paper.
Document ID
20020022031
Acquisition Source
Ames Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Murman, Scott M.
(Eloret Corp. Moffett Field, CA United States)
Chaderjian, Neal M.
(NASA Ames Research Center Moffett Field, CA United States)
Pandya, Shishir
(NASA Ames Research Center Moffett Field, CA United States)
Kwak, Dochan
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: 40th AIAA Aerosciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 1, 2002
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
PROJECT: RTOP 725-09-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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