Application of Volterra functions to X-31 aircraft model motion

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn , Issue , 2009, Pages

  Jirásek, Adam ^a,b   Cummings, Russell M ^a,b  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

^b Department of Aeronautics ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MODELS; COMPUTATIONAL FLUID DYNAMICS; FLIGHT CONTROL SYSTEMS; FORECASTING; RESEARCH AIRCRAFT; TRAINING AIRCRAFT;

AERODYNAMIC CHARACTERISTICS; CFD SIMULATIONS; LINEAR MOVEMENTS; PITCHING MOMENTS; PREDICTIVE MODELING; REDUCED ORDER MODELS; STABILITY AND CONTROL; WEAKLY NON-LINEAR;

AERODYNAMICS;

EID: 85067318961     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-3629     Document Type: Conference Paper

References (41)

1. Chambers, J. R. and Hall, R. M., "Historical Review of Uncommanded Lateral-Directional Motions at Transonic Conditions," Journal of Aircraft , Vol.41, No.3, May-June 2004, pp. 436-447.
2. Hall, R. M., Woodson, S. H., and Chambers, J. R., "Accomplishments of the Abrupt-Wing-Stall Program," Journal of Aircraft , Vol.42, No.3, May-June 2005, pp. 653-660.
3. Bowers, A. H., Pahle, J. W., Wilson, R. J., Flick, B. C., and Rood, R. L., "An Overview of the NASA F- 18 High Alpha Research Vehicle," NASA TM-4772, Oct. 1996.
4. Wang, K. C. and Iliff, K. W., "Retrospective and Recent Examples of Aircraft Parameter Identification at NASA Dryden Flight Research Center," Journal of Aircraft , Vol.41, No.4, July-August 2004, pp. 752-764.
5. Moses, R. W., "Fin buffeting features of an early F-22 model," AIAA Paper 2000-11695, April 2000.
6. Potoczsky, A. S. and Moses, R. W., "An analysis Method to Predict Tail Buffet Loads of Fighter Aircraft," AIAA Paper 2005-2291, April 2005.
7. Murman, M. M., Chaderjian, N. M., and Pandya, S. A., "Automation of a Navier-Stokes S&C database generation for the Harrier in ground effect," AIAA Paper 2002-259, 2002.
8. Chaderjian, N. M., Ahmad, J., Pandya, S., and Murman, S., "Progress Toward Generation of a Navier-Stokes Database for a Harrier in Ground Effect," AIAA Paper 2002-5966, 2002.
9. Rogers, S. E., Aftomis, M. J., Pandya, S. A., Chaderjian, N. M., Tejnil, E. T., and Ahmad, J. U., "Automated CFD Parameter Studies on Distributed Parallel Computers," AIAA Paper 2003-4229, June 2003.
10. Görtz, S., McDaniel, D., and Morton, S., "Towards an Efficient Aircraft Stability and Control Analysis Capability Using High-Fidelity CFD," AIAA-2007-11053, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 8-11, 2007.
11. Matthews, L. L. and Schwartz, M. S., "odeling and Simulations of a Dynamic Maneuvering F-16," AIAA Student Conference, May, 2008.
12. Jeans, T., McDaniel, D., Cummings, R., and Bergeron, K., "Lower-Order Aerodynamic Loads Modeling of a Maneuvering Generic Fighter Using DDES Simulations," AIAA-2009-10094, 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition, Orlando, Florida, Jan. 5-8, 2009.
13. Silva, W. A., "Identification of Nonlinear Aeroelastic Systems based of the Volterra Theory: Progress and Opportunities," Nonlinear Dynamics, Springer, Vol.39, No.9, Sept. 2005.
14. Kvaternik, R. D. and Silva, W. A., "A Computational Procedure for Identifying Bilinear Representations of Nonlinear Systems Using Volterra Kernels," NASA/TM-2008-215320, June 2008.
15. Beran, P. S., Lucia, D. J., and Pettit, C. L., "Reduced-order modelling of limit-cycle oscillation for aeroelastic systems," Journal of Fluids and Structures, Vol.19, Sept. 2004.
16. Lucia, D. J. and Beran, P. S., "Reduced-Order Model Development Using Proper Orthogonal Decomposition and Volterra Theory," AIAA Journal , Vol.42, No.6, June 2005.
17. Silva, W. A., "Discrete-Time Linear and Nonlinear Aerodynamic Impulse Responses for Efficient CFD analysis," PhD Dissertation, Faculty of the Department of Applied Science, The College of William and Mary in Virginia, VA, Sept. 1997.
18. Strang, W. Z., Tomaro, R. F., and Grismer, M. J., "The Defining Methods of Cobalt: A Parallel, Implicit, Unstructured Euler/Navier- Stokes Flow Solver," AIAA Paper 99-0786, Jan. 1999.
19. Tomaro, R. F., Strang, W. Z., and Sankar, L. N., "An implicit algorithm for solving time dependent flows on unstructured grids," AIAA Paper 1997-10333, Jan. 1997.
20. Grismer, M. J., Strang, W. Z., Tomaro, R. F., and Witzemman, F. C., "Cobalt: A Parallel, Implicit, Unstructured Euler/Navier-Stokes Solver," Adv. Eng. Software, Vol.29, No.3-6, June 1998.
21. Karypis, G., Schloegel, K., and Kumar, V., "Parmetis: Parallel Graph Partitioning and Sparse Matrix Ordering Library, Version 3.1," Technical report, Dept. Computer Science, University of Minnesota, 2003.
22. Morton, S., McDaniel, D., and Cummings, R., "F-16XL Unsteady Simulations for the CAWAPI Facet of RTO Task Group AVT-113," AIAA-2007-2493, 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 8-11, 2007.
23. Dean, J., Morton, S., McDaniel, D., and Görtz, S., "Efficient High Resolution Modeling of Fighter Aircraft with Stores for Stability and Control Clearance," AIAA-2007-11652, U.S. Air Force TandE Days, Destin, Florida, Feb. 13-15, 2007.
24. Morton, S., McDaniel, D., Dean, J., Clifton, J., and Bodkin, D., "Aircraft Stability and Control Characteristics Determined by System Identification of CFD Simulations," AIAA-2008-6378, AIAA Atmospheric Flight Mechanics Conference and Exhibit, Honolulu, Hawaii, Aug. 18-21, 2008.
25. Jeans, T., McDaniel, D., Cummings, R., and Mason, W., "Aerodynamic Analysis of a Generic Fighter Using Delayed Detached-Eddy Simulation," accepted for publication in the Journal of Aircraft, 2009.
26. Powers, S. A. and Shellenger, H. G., "The X-31 - High performance at low cost," AIAA Paper 1989-2122, AHS and ASEE Aircraft Design, Systems and Operations Conference, Seattle, WA, July 31-Aug 2, 1989, 1989.
27. Ross, H. and Robinson, M., "X-31: 20 Years of Successful International Cooperation," AIAA 2003-2572, AIAA/ICAS International Air and Space Symposium and Exposition: The Next 100 Years, 14-17 July 2003, Dayton, Ohio, 2003.
28. Tamrat, B., "A Post-Stall Technology (PST) Fighter Close-In-Combat Results Assessment, And A Look At New CIC Performance Evaluation Metric," AIAA Paper 2004-5173, AIAA Atmospheric Flight Mechanics Conference and Exhibit, Providence, Rhode Island, Aug. 16-19, 2004, 2004.
29. Canter, D. E. and Groves, A. W., "X-31 post-stall envelope expansion and tactical utility testing," AIAA Paper 1994-2171, Biennial Flight Test Conference, 7th, Colorado Springs, CO, June 20-23, 1994, Technical Papers (A94-28370 09-01), Washington, DC, American Institute of Aeronautics and Astronautics, 1994, 1994.
30. Alcorn, C. W., Croom, M. A., and Francis, M. S., "The X-31 experience - Aerodynamic impediments to post-stall agility," AIAA Paper 1995-362, Aerospace Sciences Meeting and Exhibit, 33rd, Reno, NV, Jan 9-12, 1995, 1995.
31. Grohs, T., Fischer, B., Heinzinger, O., and Brieger, O., "X-31 VECTOR - ESTOL to the Ground Flight Test Results and Lessons Learned," AIAA Paper 2004-5029, AIAA Guidance, Navigation, and Control Conference and Exhibit, 16-19 August 2004, Providence, Rhode Island, 2004.
32. Rohlf, D., Brieger, O., and Grohs, T., "X-31 VECTOR System Identification - Approach and Results," AIAA Paper 2004-4830, AIAA Atmospheric Flight Mechanics Conference and Exhibit, 16-19 August 2004, Providence, Rhode Island, 2004.
33. Young, J., "X-31 VECTOR Program Summary," AIAA Paper 2004-5026,AIAA Guidance, Navigation, and Control Conference and Exhibit, Providence, Rhode Island, Aug. 16-19, 2004, 2004.
34. Williams, D. L., Nelson, R. C., and Fisher, D., "An investigation of X-31 roll characteristics at high angle-of-attack through subscale model testing," AIAA Paper 1994-806, Aerospace Sciences Meeting and Exhibit, 32nd, Reno, NV, Jan 10-13, 1994, 1994.
35. Rein, M., Höler, G., Schütte, A., Bergmann, A., and Löser, T., "Ground-based simulation of complex maneuvers of a delta-wing aircraf," AIAA Paper 2006-3149, 25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 5-8 June 2006, San Francisco, California, 2006.
36. Schütte, A., Einarsson, G., Raichle, A., Schöning, B., Orlt, M., Neumann, J., Arnold, J., Mönnich, W., and Forkert, T., "Numerical Simulation of Maneuvering Aircraft by Aerodynamic, Flight Mechanics and Structural Mechanics Coupling," AIAA Paper 2007-1070, 45th AIAA Aerospace Sciences Meeting and Exhibit, 8-11 January 2007, Reno, Nevada, 2007.
37. Boelens, O. J., "CFD analysis of the flow around the X-31 aircraft at high angle of attack," submitted to the 27th AIAA Applied Aerodynamics Conference, 22-25 June 2009, San Antonio, TX, USA, 2009.
38. Tyssel, L., "Hybrid Grid Geeneration for complex 3D Geometries," Proceedings of the 7th International Conference on Numerical Grid Generation in Computational Field Simulation, 337-346, Whistler, British Columbia, Canada, Sept. 2000.
39. Tyssel, L., "The TRITET Grid Generation System," International Society of Grid Generation (ISGG), Proceedings of the 10th International Conference on Numerical Grid Generation in Computational Field Simulations, Forth, Crete, Greece, Sept. 2000.
40. Löser, T., "RTO/AVT-161: Assessment of Stability and Control Prediction Methods for NATO Air and Sea Vehicles Thomas Lser, DNW-NWB, X-31 Steady state and dynamic wind tunnel tests," NATO RTO AVT-113 presentation, May 2008.
41. Jirásek, A. and Cummings, R. M., "Assessment of sting effect on X-31 aircraft model using CFD," NATO-RTO AVT-161 report, to be published, 2010.