A reduced-order model for LCO dependence on mach number in F16 flight tests

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

Volumn , Issue , 2008, Pages

  Nayfeh, Ali H ^a,d   Hajjt, Muhammad R ^a,d   Nayfeh, Samir A ^b   Chabalko, Christopher C ^c,d   Beran, Philip S ^c,d  

^a VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^b Equilibria Corp   (United States)

^c AIR FORCE RESEARCH LABORATORY   (United States)

^d Department of Engineering Science and Mechanics ^*

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL NONLINEARITIES; DATA REDUCTION; DROPS; FIGHTER AIRCRAFT; MACH NUMBER; STRUCTURAL DYNAMICS; SUPERSONIC AIRCRAFT;

AERODYNAMIC NON-LINEARITIES; FLIGHT TEST; NON-LINEAR PARAMETERS; NONLINEAR COEFFICIENT; NORMAL FORM; REDUCED ORDER MODELS; TEST DATA; TRANSONIC REGIME;

AERODYNAMICS;

EID: 77957787567     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-1755     Document Type: Conference Paper

References (5)

1. C. M. Denegri "Limit Cycle Oscillation Flight Test Results of a Fighter with External Stores", Journal of Aircraft, vol. 37, No. 5, 2000, 761-769.
2. C. M. Denegri, J. A. Dubben and D. L. Maxwell "In-Flight Wing Deformation Characteristics During Limit Cycle Oscillations", Journal of Aircraft, vol. 42, No. 2, 2005, 500-508.
3. W. Silva, M. Brenner, J. Cooper, C. Dengri, S. Dunn, L. Hatsell, I. Kaynes, R. Lind, D. Poirel, and R. Yurkovich "Advanced Flutter and LCO Prediction Tools for Flight Test Risk and Cost Reduction - An International Collaborative Program for T & E Support" AIAA 2005-7630 U.S. Air Force T & E Days, Nashville, TN., 6-8 December 2005.
4. C. A. Dreyer and D. L. Shoch "F-16 flutter testing at Eglin Air Force Base", AIAA-1986-9819, AHS, CASI, DGLR, IES, ISA, ITEA, SETP, and SFTE 3rd Flight Testing Conference, Las Vegas, NV.
5. A. H. Nayfeh and Balakumar Balachandran, Applied Nonlinear Dynamics, Wiley-Interscience, New York, 1995