F-16 ventral fin buffet alleviation using piezoelectric actuators

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn , Issue , 2009, Pages

  Browning, Joseph S ^a   Cobb, Richard G ^a   Canfield, Robert A ^a   Miller, Sean K ^a  

^a AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTIVE CONTROL; AIR FORCE INSTITUTE OF TECHNOLOGIES; AIR FORCE RESEARCH LABORATORY; AIRCRAFT STRUCTURE; CONDUCTING TESTS; FLIGHT TEST; FLIGHT TESTING; GROUND TESTS; HARDWARE DESIGN; INDUCED VIBRATIONS; INFRA-RED FOR NIGHT; LEADING EDGE; LOW ALTITUDES; MODAL VIBRATIONS; PAPER DOCUMENTS; PASSIVE METHODS; STRUCTURAL ENHANCEMENTS; STRUCTURAL FAILURE; UNITED STATES AIR FORCE;

AIR NAVIGATION; AIRCRAFT; AIRCRAFT MANUFACTURE; AIRFRAMES; COMBINATORIAL OPTIMIZATION; FINS (HEAT EXCHANGE); FRACTURE MECHANICS; MILITARY AVIATION; PIEZOELECTRICITY; RESEARCH LABORATORIES; STRUCTURAL DYNAMICS; SURFACE STRUCTURE;

PIEZOELECTRIC ACTUATORS;

EID: 84855623843     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. Goh, C. J. and T. K. Caughey. "On the Stability Problem Caused by Finite Actuator Dynamics in the Collocated Control of Large Space Structures". International Journal of Control, Vol. 41(No. 3):787-802, 1985.
2. Connolly, A. J., M. Green, J. F. Chicharo, and R. R. Bitmead. "The Design of LQG & H(infinity) Controllers for use in Active Vibration Control & Narrow Band Disturbance Rejection". Proc. of the 34th Conference on Decision and Control, New Orleans, LA, 2982-2987, December 1995.
3. Burnham, J. K., D. M. Pitt., E. V. White, D. A. Henderson, and R. W. Moses. "An Advanced Buffet Load Alleviation System". 42nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, Seattle, WA, (AIAA-2001-1666), April 16-19 2001.
4. Sheta, Essam F. et al. An Active Smart Material Control System for F/A-18 Buffet Alleviation. Technical report, International Forum on Aeroelasticity and Structural Dynamics, Amsterdam, Netherlands, June 2003.
5. Hanagud, Sathyanaraya. F-15 Tail Buffet Alleviation: A Smart Structures Approach. Technical report, School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA 30332, December 1998.
6. van Tongeren, J.H., C.J. Lof, J.J. Meijer, and E.G.M. Geurts. F-16 Ventral Fins Analysis. Technical Report NLR-CR-99366, National Aerospace Laboratory, Amsterdam, The Netherlands, August 1999.
7. Lazarus, K. B., E. Saarmaa, and G. S. Agnes. "An Active Smart Material System for Buffet Load Alleviation". SPIE's 2nd Annual International Symposium on Smart Structures and Materials, Vol. 2447:179-192, 1995.
8. Moses, Robert W. NASA Langley Research Center's Contributions to International Active Buffet Alleviation Programs. Technical report, Aeroelasticity Branch, NASA Langley Research Center, Hampton, VA, 1999.
9. Falangas, Eric T. et al. Piezoceramic Actuator Active Vibration Suppression System B-1B Flight Demonstration Program. Technical Report AFRL-VA-WP-TR-1999-3011, Air Vehicles Directorate, Air Force Research Laboratory, AFMC, Wright-Patterson AFB, Ohio, January 1998.
10. Morgenstern, Shawn D., Alleviation of Buffet-Induced Vibration using Piezoelectric Actuators. Masters thesis, Graduate School of Engineering, Air Force Institute of Technology, Wright-Patterson AFB, OH, Febuary 2006, AFIT/GAE/ENY/06-M25.
11. Morgenstern, Shawn D., Aaron A. Tucker, Heather C. Giebner, Aniello Violetti, and Dick Wong. Limited Characterization of Dual Bimorph Synthetic Jet Actuators: Aeroelastic Load Control - Phase I, Project HAVE PUFF. Technical Information Memorandum AFFTC-TIM-05-07, Air Force Flight Test Center, Edwards AFB, CA 93524, December 2005.
12. nd edition, 2002.