Coupled and uncoupled bending-torsion responses of twin-tail buffet

Journal of Fluids and Structures

Volumn 12, Issue 6, 1998, Pages 677-701

  Kandil, O A ^a   Sheta, E F ^a  

^a Old Dominion University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0000572894     PISSN: 08899746     EISSN: None     Source Type: Journal    
DOI: 10.1006/jfls.1998.0168     Document Type: Article

References (13)

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2. COLE, S. R., MOSS, S. W. & DOGGET, R. V., Jr 1990 Some buffet response characteristics of a twin-vertical-tail configuration. NASA TM-102749.
3. ERICKSON, G. E., HALL, R. M., BANKS, D. W., DEL FRATE, J. H., SHREINER, J. A., HANLEY, R. J. & PULLEY, C. T. 1989 Experimental investigation of the F/A-18 vortex flows at subsonic through transonic speeds. AIAA Paper 89-2222.
4. KANDIL, O. A., KANDIL, H. A. & MASSEY, S. J. 1993 Simulation of tail buffet using delta wing-vertical tail configuration. AIAA Paper 93-3688-CP, AIAA Atmospheric Flight Mechanics Conference, Montery, CA, U.S.A., pp. 566-577.
5. KANDIL, O. A., MASSEY, S. J., & KANDIL, H. A., 1994 Computations of vortex-breakdown induced tail buffet undergoing bending and torsional vibrations. AIAA Paper 94-1428-CP, AIAA/ASME/ASCE/ASC Structural, Structural Dynamics and Materials Conference, Hilton Head SC, U.S.A. pp. 977-993.
6. KANDIL, O. A., MASSEY, S. J. & SHETA, E. F., 1995 Structural dynamics/CFD interaction for computation of vertical tail buffet. International Forum on Aeroelasticity and Structural Dynamics, Royal Aeronautical Society, Manchester, U.K., 26-28 June, pp. 52.1-52.14. Also published in the journal of the Royal Aeronautical Society, August/September 1996, pp. 297-303.
7. KANDIL, O. A., MASSEY, S. J. & SHETA, E. F., 1995 Structural dynamics/CFD interaction for computation of vertical tail buffet. International Forum on Aeroelasticity and Structural Dynamics, Royal Aeronautical Society, Manchester, U.K., 26-28 June, pp. 52.1-52.14. Also published in the journal of the Royal Aeronautical Society, August/September 1996, pp. 297-303.
8. KANDIL, O. A., SHETA, E. F. & LIU, C. H., 1996 Computation and validation of fluid/structure twin-tail buffet response. Euromech Colloquium 349, Structure-Fluid Interaction in Aeronautics, Institut für Aeroelastik, Göttingen, Germany.
9. KANDIL, O. A., SHETA, E. F. & MASSEY, S. J., 1997 Fluid/Structure twin tail buffet response over a wide range of angles of attack. AIAA Paper 97-2261-CP, 15th AIAA Applied Aerodynamics Conference, Atlanta, GA, U.S.A.
10. LEE, B. & BROWN, D., 1990 Wind tunnel studies of F/A-18 tail buffet. AIAA Paper 90-1432.
11. SELLERS, W. L. III, MEYERS, J. F. & HEPNER, T. E., 1988 LDV survey over a fighter model at moderate to high angle of attack. SAE Paper 88-1448.
12. WASHBURN, A. E., JENKINS, L. N. & FERMAN, M. A., 1993 Experimental investigation of vortex-fin interaction. AIAA Paper 93-0050, Reno, NV, U.S.A.
13. WENTZ, W. H., 1987 Vortex-Fin interaction on a fighter aircraft. AIAA Paper 87-2474, AIAA Fifth Applied Aerodynamics Conference, Monterey, CA, U.S.A.