Virtual aeroelastic flight testing for the F-16 fighter with stores

Collection of Technical Papers - U.S. Air Force T and E Days, 2007(Test and Evaluation

Volumn , Issue , 2007, Pages 339-346

  Thomas, Jeffrey P ^a,c,d   Dowels, Earl H ^a,c,d,e   Hall, Kenneth C ^a,c,d   Denegri Jr , Charles M ^b,d,f  

^a DUKE UNIVERSITY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c Department of Mechanical Engineering and Materials Science ^*

^d AIAA   (United States)

^e School of Engineering

^f Engineering Division

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTIC FLIGHT TESTING; AEROELASTIC FLUTTER; COMPUTATIONAL FLUID DYNAMIC FLOW SOLVER; WINGTIP LAUNCHERS;

COMPUTATIONAL FLUID DYNAMICS; FIGHTER AIRCRAFT; FLUTTER (AERODYNAMICS); MISSILES; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER;

SPACE FLIGHT;

EID: 35648947921     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (17)

1. Thomas, J. P., Dowell, E. H., Hall, K. C., and Denegri, C. M., "An Investigation of the Sensitivity of F-16 Fighter Limit Cycle Oscillations to Uncertainties," AIAA Paper 2006-1847, 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials (SDM) Conference, Newport, RI.
2. Thomas, J. P., Dowell, E. H., Hall, K. C., and Charles M. Denegri, J., "Further Invesitgation of Modeling Limit Cycle Oscillation Behavior of the F-16 Fighter Using a Harmonic Balance Approach," AIAA Paper 2005-1917, Presented at the 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials (SDM) Conference, Austin, TX.
3. Thomas, J. P., Dowell, E. H., Hall, K. C., and Charles M. Denegri, J., "Modeling Limit Cycle Oscillation Behavior of the F-16 Fighter Using a Harmonic Balance Approach," AIAA Paper 2004-1696, Presented at the 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials (SDM) Conference, Palm Springs, CA.
4. HaIl, K. C., Thomas, J. P., and Clark, W. S., "Computation of Unsteady Nonlinear Flows in Cascades Using a Harmonic Balance Technique," AIAA Journal, Vol. 40, No. 5, May 2002, pp. 879-886.
5. Thomas, J. P., Dowell, E. H., and Hall, K. C., "Nonlinear Inviscid Aerodynamic Effects on Transonic Divergence, Flutter and Limit Cycle Oscillations," AIAA Journal, Vol. 40, No. 4, April 2002, pp. 638-646.
6. Thomas, J. P., Dowell, E. H., and Hall, K. C., "Modeling Viscous Transonic Limit Cycle Oscillation Behavior Using a Harmonic Balance Approach," AIAA Paper 2002-1414.
7. Thomas, J. P., Dowell, E. H., and Hall, K. C., "A Harmonic Balance Approach for Modeling Three-Dimensional Nonlinear Unsteady Aerodynamics and Aeroelasticity," ASME Paper IMECE-2002-32532.
8. Charles M. Denegri, J. and Dubben, J. A., "F-16 Limit Cycle Oscillation Analysis Using Transonic Small-disturbance Theory," AIAA Paper 2005-2296, Presented at the 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials (SDM) Conference, Austin, TX.
9. Charles M. Denegri, J. and Dubben, J. A., "In-Flight Wing Deformation Characteristics During Limit Cycle Oscillations," AIAA Paper 2003-1426.
10. Charles M. Denegri, J., "Limit Cycle Oscillation Flight Test Results of a Fighter with External Stores," Journal of Aircraft, Vol. 37, No. 5, 2000, pp. 761-769.
11. Parker, G. H., Maple, R. C., and Beran, P. S., "Analysis of Store Effects on Limit-Cycle Oscillation," AIAA Paper 2006-1846, Presented at the 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials (SDM) Conference, Newport, RI.
12. Parker, G. H. and Maple, R. C., "The Role of Viscosity in Store-Induced Limit-Cycle Oscillation," AIAA Paper 2005- 1916, Presented at the 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials (SDM) Conference, Austin, TX.
13. Lieu, T. and Farhat, C., "Adaptation of Pod-Based Aeroelastic ROMs for Varying Mach Number and Angle of Attack: Application to a Complete F-16 Configuration," AIAA Paper 2005-7666, U.S. 2005 Air Force T&E Days, Nashville, TN.
14. Lieu, T., Farhat, C., and Lesoinne, M., "POD-based Aeroelastic Analysis of a Complete F-16 Configuration: ROM Adaptation and Demonstration," AIAA Paper 2005-2295.
15. Prananta, B. B., Kok, J. C., Spekreijse, S. P., Hounjet, M. H. L., and Meijer, J. J., "Simulation of Limit Cycle Oscillation of Fighter Aircraft at Moderate Angle of Attack," Tech. Rep. NRL-TP-2003-526, National Aerospace Laboratory NRL, 2003.
16. Melville, R., "Nonlinear Mechanisms of Aeroelastic Instability for the F-16," AIAA Paper 2002-0871.
17. Bisplinghoff, R. L., Ashley, H., and Halfman, R. L., Aeroelasticity, Dover Science Books, 1996.