NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Towards Distributed Fluids/Controls SimulationsComputational prototyping of aircraft in nonlinear regimes will require the coupling of high-order disciplines on high performance computers. This effort investigates the coupling of the Reynolds-averaged Navier-Stokes equations with six degree-of-freedom nonlinear body dynamics and controls on distributed architectures. Towards this goal, solutions obtained on a wide-node IBM SP-2, an Ethernet-linked cluster of workstations, and a Cray C90 are compared in terms of accuracy and throughput.
Document ID
19990027785
Acquisition Source
Ames Research Center
Document Type
Reprint (Version printed in journal)
Authors
Atwood, Christopher A.
(Overset Methods, Inc. Moffett Field, CA United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1995
Subject Category
Computer Programming And Software
Meeting Information
Meeting: Computational Aerosciences
Location: Santa Clara, CA
Country: United States
Start Date: March 1, 1995
Sponsors: NASA Headquarters
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available