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Computational Methods for Stability and Control (COMSAC): The Time Has ComePowerful computational fluid dynamics (CFD) tools have emerged that appear to offer significant benefits as an adjunct to the experimental methods used by the stability and control community to predict aerodynamic parameters. The decreasing costs for and increasing availability of computing hours are making these applications increasingly viable as time goes on and the cost of computing continues to drop. This paper summarizes the efforts of four organizations to utilize high-end computational fluid dynamics (CFD) tools to address the challenges of the stability and control arena. General motivation and the backdrop for these efforts will be summarized as well as examples of current applications.
Document ID
20050207434
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Hall, Robert M.
(NASA Langley Research Center Hampton, VA, United States)
Biedron, Robert T.
(NASA Langley Research Center Hampton, VA, United States)
Ball, Douglas N.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Bogue, David R.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Chung, James
(Naval Air Systems Command Patuxent River, MD, United States)
Green, Bradford E.
(Naval Air Systems Command Patuxent River, MD, United States)
Grismer, Matthew J.
(Air Force Research Lab. Wright-Patterson AFB, OH, United States)
Brooks, Gregory P.
(Air Force Research Lab. Wright-Patterson AFB, OH, United States)
Chambers, Joseph R.
(Chambers Consulting Yorktown, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA Paper 2005-6121
Report Number: AIAA Paper 2005-6121
Meeting Information
Meeting: AIAA Atmospheric Flight Mechanics Conference and Exhibit
Location: San Francisco, CA
Country: United States
Start Date: August 15, 2005
End Date: August 18, 2005
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
OTHER: 23-065-30-11
Distribution Limits
Public
Copyright
Public Use Permitted.
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