High resolution simulation of full aircraft control at flight reynolds numbers

Department of Defense - Proceedings of the HPCMP Users Group Conference 2007; High Performance Computing Modernization Program: A Bridge to Future Defense, DoD HPCMP UGC

Volumn , Issue , 2007, Pages 41-47

  Morton, Scott A ^a   McDaniel, David R ^b   Bergeron, Keith ^b   Cummings, Russell M ^b   Goertz, Stefan ^b   Seidel, Jurgen ^b   Forsythe, James R ^c   Squires, Kyle D ^d  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b UNITED STATES AIR FORCE ACADEMY   (United States)

^c Cobalt Solutions LLC ^*  (United States)

^d ARIZONA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIR; AIRCRAFT; BRIDGES; CHLORINE COMPOUNDS; COMPUTATIONAL METHODS; DYNAMIC RESPONSE; ELECTRIC LOAD SHEDDING; GAS DYNAMICS; HIGH PERFORMANCE LIQUID CHROMATOGRAPHY; MODERNIZATION; REYNOLDS NUMBER; TESTING; TRANSPORT AIRCRAFT;

AERODYNAMIC DATABASES; AERODYNAMIC PHENOMENA; AIRCRAFT CONTROL; AIRCRAFT RESPONSES; COMPUTATIONAL DATA; CONTROL SURFACES; CURRENT STABILITY; DEPARTMENT OF DEFENSE; FLIGHT MANEUVERS; FLIGHT REYNOLDS NUMBERS; FLIGHT TESTING; HIGH PERFORMANCE COMPUTING MODERNIZATION PROGRAM; HIGH RESOLUTIONS; MOTION DATA; PAPER DOCUMENTS; RAPID GENERATION; REDUCED ORDER MODELLING; STATIC AND DYNAMIC; THREE-AXIS;

FLIGHT CONTROL SYSTEMS;

EID: 49949116923     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/HPCMP-UGC.2007.37     Document Type: Conference Paper

References (22)

1. Withrow, M., "Dr. Raymond Gordnier Discusses the Research Direction of Advanced Computational Methods." Air Force Research Laboratory Horizons, April 2005.
2. Johnson, F.T., E.N. Tinoco, and N.J. Yu, "Thirty Years of Development and Application of CFD at Boeing Commercial Airplanes, Seattle." AIAA Paper 2003-3439, 16th AIAA Computational Fluid Dynamics Conference, Orlando, FL, June 2003.
3. Strang, W.Z., R.F. Tomaro, and M.J. Grismer, "The defining methods of Cobalt60: a parallel, implicit, unstructured Euler/Navier-Stokes flow solver." AIAA Paper 1999-0786, 1999.
4. Tomaro, R.F., W.Z. Strang, and L.N. Sankar, "An implicit algorithm for solving time dependent flows on unstructured grids." AIAA Paper 1997-0333, 1997.
5. Grismer, M.J., W.Z. Strang, R.F. Tomaro, and F.C. Witzemman, "Cobalt: A Parallel, Implicit, Unstructured Euler/Navier-Stokes Solver." Adv. Eng. Software, Vol. 29, No. 3-6, pp. 365-373, 1998.
6. Karypis, G., K. Schloegel, and V. Kumar, "Parmetis: Parallel Graph Partitioning and Sparse Matrix Ordering Library, Version 3.1." Technical report, Dept. Computer Science, University of Minnesota, 2003.
7. Spalart, P.R., S. Deck, M.L. Shur, K.D. Squires, M.Kh. Strelets, and A. Travin, "A New Version of Detached-Eddy Simulation. Resistant to Ambiguous Grid Densities." Theoretical Computational Fluid Dynamics, Vol. 20, pp. 181-195, 2006.
8. Ljung, L., System Identification. Theory for the User, Prentice Hall Information and System Sciences Series.
9. Morelli, E.A. and V. Klein, "Application of System Identification to Aircraft at NASA Langley Research Center." Journal of Aircraft, Vol. 42, No. 1, pp. 12-25, January-February 2005.
10. Klein, V. and E.A. Morelli, "Aircraft System Identification - Theory and Practice." AIAA Educational Series, 2006.
11. Jategaonkar, R.V., "Flight Vehicle System Identification - A Time Domain Methodology." Progress in Astronautics and Aeronautics, Vol. 216, F.K. Lu, editor, AIAA, 2006.
12. Jategaonkar, R.V., D. Fischenberg, and W. Gruenhagen, "Aerodynamic Modeling and System Identification from Flight Data - Recent Applications at DLR." Journal of Aircraft 2004, 0021-8669, vol.41, no.4, pp. 681-69, 2004.
13. Morelli, E.A., "Global Nonlinear Parametric Modeling with Application to F-16 Aerodynamics." ACC Paper WP04-2, Paper ID i-98010-2, American Control Conference, Philadelphia, Pennsylvania, June 1998.
14. Morton, S., S. Goertz, and D. McDaniel, "Computational Aircraft and Armament Stability and Control Techniques Applied to the F-16." ITEA Store Compatibility Symposium, Destin, FL, April 2006.
15. Morton, S.A., J. Dean, D.R. McDaniel, and S. Görtz, "Poster Paper on Computational Aircraft and Armament Stability and Control Techniques Applied to the F-16." International Test and Evaluation Association National Symposium, Orlando, FL, November 2006.
16. Morton, S.A., S. Görtz, D.R. McDaniel, "Computational Stability and Control Analysis of the F-16." Maui High Performance Computing Center Application Briefs, 2006.
17. Morton, S.A., McDaniel, D.R., and Cummings, R.M., "F-16XL Unsteady Simulations for the CAWAPI Facet of RTO Task Group AVT- 113." AIAA Paper 2007-0493, Aerospace Sciences Meeting, Reno, NV, January 2007.
18. Görtz, S., D.R. McDaniel, and S.A. Morton, "Towards an Efficient Aircraft Stability and Control Analysis Capability using High-Fidelity CFD." AIAA Paper 2007-1053, Aerospace Sciences Meeting, Reno, NV, January 2007.
19. Dean, J., S.A. Morton, D.R. McDaniel, and S. Görtz., "Efficient High Resolution Modeling of Fighter Aircraft with Stores for Stability and Control Clearance." AIAA Paper 2007-1652, American Institute of Aeronautics and Astronautics Air Force Test and Evaluation Days Conference, Sandestin, FL, April 2007.
20. Samareh, S., "GridTool: A Surface Modeling and Grid Generation Tool, Proceedings of the Workshop on Surface Modeling, Grid Generation, and Related Issues in CFD Solutions." NASA CP-3291, May 9-11, 1995.
21. Pirzadeh, S., "Progress Toward A User-Oriented Unstructured Viscous Grid Generator." AIAA Paper 96-0031, 1996.
22. Blacksmith User's Manual, Cobalt Solutions, Version 3.0, 2005.