Active smart material control system for buffet alleviation

Journal of Sound and Vibration

Volumn 292, Issue 3-5, 2006, Pages 854-868

  Sheta, Essam F ^a   Moses, Robert W ^b   Huttsell, Lawrence J ^c  

^a CFD RESEARCH CORPORATION   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BENDING (DEFORMATION); ELECTRODYNAMICS; FATIGUE OF MATERIALS; FIGHTER AIRCRAFT; PIEZOELECTRIC DEVICES; STRUCTURAL ANALYSIS; SYNCHRONIZATION;

BUFFET ALLEVIATION; FLUID-STRUCTURE INTERFACES; HIGH-FIDELITY ANALYSIS;

BUFFETING;

EID: 33644592638     PISSN: 0022460X     EISSN: 10958568     Source Type: Journal    
DOI: 10.1016/j.jsv.2005.09.002     Document Type: Article

References (22)

1. B. Lee, D. Brown, M. Zgela, D. Poirel, Wind tunnel investigation of tail buffet on the F-18 aircraft, AGARD-CP-483, 1990.
2. L.A. Meyn, K.D. James, Full scale wind tunnel studies of F/A-18 tail buffet, AIAA Paper 93-3519, 1993.
3. C. Pettit, D. Brown, E. Pendleton, Wind tunnel tests of full-scale F/A-18 twin tail buffet: a summary of pressure and response measurements, AIAA Paper 94-3476, 1994.
4. R.W. Moses, L.J. Huttsell, Fin buffeting features of an early F-22 model, AIAA Paper 2000-1695, 2000.
5. E.F. Sheta, L.J. Huttsell, Numerical analysis of F/A-18 vertical tail buffeting, AIAA Paper 2001-1664, 2001.
6. G.H. Shah, Wind-tunnel investigation of aerodynamic and tail buffet characteristics of leading-edge extension modifications to the F/A-18, AIAA Paper 91-2889, 1991.
7. B. Lee, N. Valerio, Vortical flow structure near the F/A-18 LEX at high incidence, Journal of Aircraft (1994) 1221-1223.
8. D. Rao, C. Puram, G. Shah, Vortex control for tail buffet alleviation on a twin-tail fighter configuration, SAE Paper 892221, 1989.
9. E.F. Sheta, Buffet alleviation of F/A-18 aircraft using LEX fences, AIAA Paper 2003-1888, 2003.
10. E.F. Sheta, L.J. Huttsell, Control of F/A-18 vertical tail buffeting by vortical blowing, AIAA Paper 2002-0948, 2002.
11. E.F. Sheta, V.J. Harrand, L.J. Huttsell, Active vortical flow control for alleviation of twin-tail buffet of generic fighter aircraft, Journal of Fluids and Structures (2001) 769-789.
12. H. Ashley, H. Rock, R. Digumarthi, K. Chaney, A. Eggers, Active control for fin buffet alleviation, WL-TR-93-3099, 1994.
13. R.W. Moses, Active vertical tail buffeting alleviation on an F/A-18 model in a wind tunnel, Second Joint NASA/FAA/DOD Conference on Aging Aircraft, Williamsburg, VA, 1998.
14. R.W. Moses, Vertical tail buffeting alleviation using piezoelectric actuators - some results of the actively controlled response of buffet-affected tails (ACROBAT) program, NASA TM 110336, 1997.
15. R.W. Moses, C.D. Wiesman, A.A. Bent, A.E. Pizzochero, Evaluation of new actuators in a buffet loads environment, CEAS/AIAA/AIAE International Forum on Aeroelasticity and Structural Dynamics, Madrid, Spain, 2001.
16. G.M. Kingsley, J.M. Siegel, V.J. Harrand, C. Lawrence, J. Luker, Development of the multi-disciplinary computing environment (MDICE), AIAA Paper 98-4738, 1998.
17. E.F. Sheta, Prediction and control of twin-tail buffet of fighter aircraft, AirForce Research Laboratory Technical Report AFRL-VA-WP-TR-2002-3049, 2002.
18. B. Jaffe, R. Cook, and H. Jaffe Piezoelectric Ceramics 1971 Academic Press New York, NY
19. J.F. Thompson, B.K. Soni, and N.P. Weatherill Handbook of Grid Generation 1998 CRC Press Boca Raton, FL pp.3.1-3.15
20. W.K. Wilkie, R.G. Bryant, J.W. High, R.L. Fox, R.F. Hellbaum, A. Jalink, B. Little, P. Mirick. Low-cost piezocomposite actuator for structural control applications, SPIE Seventh International Symposium on Smart Structures and Materials, 2000.
21. M.S. Azzouz, J.S. Bevan, J.J. Ro, C. Mei, Finite element modeling of MFC/AFC actuators, SPIE Eighth International Symposium on Smart Structures and Materials, 2001.
22. L.A. Meyn, K.D. James, R.J. Green, Correlation of F/A-18 tail buffet results, High Alpha Projects and Technology Conference, Dryden Flight Research Center, 1994.