Computations on Wings With Full-Span Oscillating Control Surfaces Using Navier-Stokes Equations

Computations on Wings With Full-Span Oscillating Control Surfaces Using Navier-Stokes Equations

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Publisher's Synopsis

A dual-level parallel procedure is presented for computing large databases to support aerospace vehicle design. This procedure has been developed as a single Unix script within the Parallel Batch Submission environment utilizing MPIexec and runs MPI based analysis software. It has been developed to provide a process for aerospace designers to generate data for large numbers of cases with the highest possible fidelity and reasonable wall clock time. A single job submission environment has been created to avoid keeping track of multiple jobs and the associated system administration overhead. The process has been demonstrated for computing large databases for the design of typical aerospace configurations, a launch vehicle and a rotorcraft. Guruswamy, Guru P. Ames Research Center NASA/TM-2013-216601, ARC-E-DAA-TN11370

Book information

ISBN: 9781794397019
Publisher: Amazon Digital Services LLC - KDP Print US
Imprint: Independently Published
Pub date:
Language: English
Number of pages: 30
Weight: 95g
Height: 279mm
Width: 216mm
Spine width: 2mm