Numerical analysis of store-induced limit-cycle oscillation

Journal of Aircraft

Volumn 41, Issue 6, 2004, Pages 1315-1326

  Beran, P S ^a   Khot, N S ^a   Eastep, F E ^a   Snyder, R D ^a   Zweber, J V ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BIFURCATION (MATHEMATICS); COMPUTER SIMULATION; MATHEMATICAL MODELS; NUMERICAL ANALYSIS; REYNOLDS NUMBER; WINGS;

COORDINATES; ELASTIC AXIS; FREESTREAM CONDITIONS; MACH NUMBER;

OSCILLATIONS;

EID: 10944233712     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.404     Document Type: Article

References (26)

1. Denegri, C. M., "Limit Cycle Oscillation Flight Test Results of a Fighter with External Stores," Journal of Aircraft, Vol. 37, No. 5, 2000, pp. 761-769.
2. Turner, C. D., "Effect of Store Aerodynamics on Wing/Store Flutter," Journal of Aircraft, Vol. 19, No. 7, 1982, pp. 574-580.
3. Gern, F. H., and Librescu, L., "Static and Dynamic Aeroelasticity of Advanced Aircraft Wings Carrying External Stores," AIAA Journal, Vol. 36, No. 7, 1998, pp. 1121-1129.
4. Eastep, F. E., and Olsen, J. J., "Transonic Flutter Analysis of a Rectangular Wing with Conventional Airfoil Sections," AIAA Journal, Vol. 17, No. 10, 1980, pp. 1159-1164.
5. Melville, R., "Nonlinear Simulation of F-16 Aeroelastic Instability," AIAA Paper 2001-0570, Jan. 2001.
6. Melville, R., "Nonlinear Mechanisms of Aeroelastic Instability for the F-16," AIAA Paper 2002-0871, Jan. 2002.
7. Farhat, C., Pierson, K., and Degand, C., "CFD Based Simulation of the Unsteady Aeroelastic Response of a Maneuvering Vehicle," AIAA Paper 2000-0899, Jan. 2000.
8. Batina, J. T., "Efficient Algorithm for Solution of the Unsteady Transonic Small-Disturbance Equation," Journal of Aircraft, Vol. 25, No. 7, 1988, pp. 598-605.
9. Batina, J. T., "Unsteady Transonic Algorithm Improvements for Realistic Aircraft Applications," Journal of Aircraft, Vol. 26, No. 2, 1989, pp. 131-139.
10. Batina, J. T., "A Finite Difference Approximate-Factorization Algorithm for Solution of the Unsteady Transonic Small-Disturbance Equation," NASA TP 3129, Jan. 1992.
11. Hewlett, J. T., "Efficient Self-Consistent Viscous Inviscid Solution for Unsteady Transonic Flow," Journal of Aircraft, Vol. 24, No. 11, 1987, pp. 737-744.
12. Edwards, J. W., "Transonic Shock Oscillations Calculated with a New Interactive Boundary Layer Coupling Method," AIAA Paper 93-0777, Jan. 1993.
13. Edwards, J. W., "Calculated Viscous and Scale Effects on Transonic Aeroelasticity," Numerical Unsteady Aerodynamic and Aeroelastic Simulation, North Atlantic Treaty Organization, AGARD-R-822, March 1998, pp. 1-1-1-11.
14. Green, J. E., Weeks, D. J., and Brooman, J. W. F., "Prediction of Turbulent Boundary Layers and Wakes in Compressible Flow by a Lag-Entrainment Method," British Aeronautical Research Council, R&M No. 3791, London, 1977.
15. Schuster, D. M., Vadyak, J., and Atta, E., "Static Aeroelastic Analysis of Fighter Aircraft Using a Three-Dimensional Navier-Stokes Algorithm," Journal of Aircraft, Vol. 27, No. 9, 1990, pp. 820-825.
16. Smith, M. J., Schuster, D. M., Huttsell, L. J., and Buxton, B., "Development of and Euler/Navier-Stokes Aeroelastic Method for Three-Dimensional Vehicles with Multiple Flexible Surfaces," AIAA Paper 96-1400, April 1996.
17. Schuster, D. M., Beran, P. S., and Huttsell, L. J., "Application of the ENS3DAE Euler/Navier-Stokes Aeroelastic Method," Numerical Unsteady Aerodynamic and Aeroelastic Simulation, North American Treaty Organization, AGARD-R-822, March 1998, pp. 3-1-3-11.
18. Lewis, A. P., and Smith, M. J., "Euler-Based Aeroelastic Analysis of Shell Structures," Journal of Aircraft, Vol. 37, No. 5, 2000, pp. 840-845.
19. Huttsell, L., Schuster, D., Volk, J., Giesing, J., and Love, M., "Evaluation of Computational Aeroelasticity Codes for Loads and Flutter," AIAA Paper 2001-0569, Jan. 2001.
20. Thomas, P. D., and Lombard, C. K., "Geometric Conservation Law and Its Application to Flow Computations on Moving Grids," AIAA Journal, Vol. 17, No. 10, 1979, pp. 1030-1037.
21. Smith, M. J., Hodges, D. H., and Cesnik, C. E. S., "An Evaluation of Computational Algorithms to Interface Between CFD and CSD Methodologies," WL-TR-96-3055, Wright-Patterson Air Force Base, Nov. 1995.
22. Smith, M. J., Hodges, D. H., and Cesnik, C. E. S., "Evaluation of Computational Algorithms Suitable for Fluid-Structure Interactions," Journal of Aircraft, Vol. 37, No. 2, 2000, pp. 292-294.
23. Beran, P. S., Khot, N. S., Eastep, F. E., Strganac, T. W., and Zweber, J. V., "Effects of Viscosity on Store-Induced Limit-Cycle Oscillation," Proceedings of the 2003 ITEA Aircraft-Stores Compatibility Symposium XIII, International Test and Evaluation Association, Fairfax, VA, Feb. 2003.
24. Tang, D., and Dowell, E. H., "Effects of Angle of Attack on Nonlinear Flutter of a Delta Wing," AIAA Journal, Vol. 39, No. 1, 2001, pp. 15-21.
25. Khot, N. S., Beran, P. S., Zweber, J. V., and Eastep, F. E., "Influence of Tip Store Mass Location on Wing Limit-Cycle Oscillation," AIAA Paper 2003-1731, April 2003.
26. Snyder, R. D., Scott, J. N., Khot, N. S., Beran, P. S., and Zweber, J. V., "Predictions of Store-Induced Limit-Cycle Oscillations Using Euler and Navier-Stokes Fluid Dynamics," AIAA Paper 2003-1727, April 2003.