Limit cycle oscillation flight test results for asymmetric store configurations

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

Volumn 1, Issue , 2003, Pages 267-277

  Dawson, Kenneth S ^a   Maxwell, Daniel L ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; FINITE ELEMENT METHOD; FLIGHT DYNAMICS; FLUTTER (AERODYNAMICS); NATURAL FREQUENCIES; OSCILLATIONS;

FULL SPAN LINEAR ANALYSIS; HALF SPAN FLUTTER ANALYSIS TECHNIQUE; LIMIT CYCLE OSCILLATIONS; TRANSONIC FLUTTER;

FIGHTER AIRCRAFT;

EID: 0042513890     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-1427     Document Type: Conference Paper

References (12)

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3. Meijer, Jos J., and Cunningham, Atlee M., Jr., "A Semi-Empirical Unsteady Nonlinear Aerodynamic Model to Predict Transonic LCO Characteristics of Fighter Aircraft," 36th Structures, Structural Dynamics, and Materials Conference, AIAA-95-1340, April 1995.
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5. Denegri, Charles M., Jr., "Limit Cycle Oscillation Flight Test Results of a Fighter with External Stores," Journal of Aircraft, Vol. 37, No. 5, September-October 2000, pp. 761-769.
6. Katz, Henry, "Flutter of Aircraft with External Stores," U.S. Air Force Aircraft/Stores Compatibility Symposium, November 1969.
7. Sensburg, O., Lotze, A. and Haidl, G., "Wing with Stores Flutter on Variable Sweep Wing Aircraft," AGARD Conference Proceedings, No. 162, October 1974.
8. Lotze, A., "Asymmetric Store Flutter," AGARD Report No. 668, April 1978.
9. Maricic, Nikola L., "Calculation of Critical Flutter Speeds of an Aircraft in Subsonic Flow,", Computers and Structures, Vol. 12, 1980, pp. 475-482.
10. Guruswamy, Guru P., and Tu, Eugene L., "Effects of Symmetric and Asymmetric Modes on Transonic Aeroelastic Characteristics of Full-Span Wing-Body Configurations," 29th Structures, Structural Dynamics, and Materials Conference, AIAA-88-2308, April 1988.
11. Dawson, Kenneth S., and Sussingham, J. Chris, "F-16 Limit Cycle Oscillation Testing with Asymmetric Stores," 17th AIAA Applied Aerodynamics Conference, AIAA-99-3142, June 1999.
12. Dreyer, Catherine A., and Shoch, David L., "F-16 Flutter Testing at Eglin Air Force Base," 3rd Flight Testing Conference, AIAA-86-9819, April 1986.