Application of OVERFLOW-MLP to the analysis of the 1303 UCAV

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn 1, Issue , 2006, Pages 483-510

  Wong, Michael D ^a,b   Flores, Jolen ^a,b  

^a NASA AMES RESEARCH CENTER   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; DATA ACQUISITION; MATHEMATICAL MODELS; PROJECT MANAGEMENT; SUPERCOMPUTERS; TURBULENCE; TURBULENT FLOW; WIND TUNNELS;

BOEING (CO); THE TECHNICAL COOPERATION PROGRAM (TTCP); TURBULENCE MODEL; TURBULENT FLOW FIELD;

REMOTELY OPERATED VEHICLES;

EID: 33845415243     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-2987     Document Type: Conference Paper

References (7)

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2. th Fluid Dynamics Conference, San Francisco, CA June 2006.
3. Bruce, R.J., Mundell, A.R.G., "Low Speed Wind Tunnel Test on the 1303 UCAV Concept", QinetiQ/FST/TR025502/1.0, QinetiQ, Ltd., Farnborough, U.K., March 2003.
4. th, Canada, 2002.
5. Gridgen, Pointwise, Inc., 22nd May 2006, http://www.pointwise.com/ gridgen.
6. Suhs, N.E., Tramel, R.W., "PEGSUS 4.0 User's Manual", Arnold Engineering Development Center, DOF, November 1991.
7. National Aeronautics and Space Administration, SGI Altix Columbia Supercomputer, 22nd May 2006, http://www.nas.nasa.gov/Resources/Systems/ columbia.html.