The role of non-linear aerodynamics in fluid-structure interaction

29th AIAA Fluid Dynamics Conference

Volumn , Issue , 1998, Pages 1-14

  Cunningham, Atlee M ^a  

^a LOCKHEED MARTIN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EQUATIONS OF MOTION; FLUID DYNAMICS; FLUID STRUCTURE INTERACTION; SWEPT WINGS; VORTEX FLOW;

AERODYNAMIC NON-LINEARITIES; LARGE AMPLITUDE; LEADING-EDGE VORTICES; LIMIT CYCLE OSCILLATION (LCO); NON-LINEAR AERODYNAMIC FORCES; NON-LINEAR AERODYNAMICS; NONLINEAR AERODYNAMIC MODEL; SOLUTION APPROACH;

AERODYNAMICS;

EID: 57649109634     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-2423     Document Type: Conference Paper

References (12)

1. Cunningham, A. M., Jr.., “Practical Problems: Airplanes”, Chapter 3, Unsteady Transonic Aerodynamics, edited by D. L. Nixon, AIM Progress in Astronautics and Aeronautics Series, 1989.
2. Cunningham, A. M., Jr. Meijer, J. J., “Semi-Empirical Unsteady Aerodynamics for Modeling Aircraft Limit Cycle Oscillations and Other Non-Linear Aeroelastic Problems”, presented at the “International Forum on Aeroelasticity and Structural Dynamics, 1995”, Manchester, U. K., 26-28 June 1995.
3. Coe, C. F. and Cunningham, A. M., Jr.., Prediction of F-111 TACT Aircraft Buffet Response and Correlations of Fluctuating Pressures Measured on Aluminum and Steel Models of the Aircraft. NASA CR-4069, May 1987.
4. Meijer, J. J., Cunningham, A. M., Jr., Zwaan, R. J., “A Semi-Empirical Approach to Predict Transonic Limit Cycle Oscillation Characteristics of Fighter Aircraft”, 8th Aircraft/ Stores Compatibility Symposium, Fort Walton Beach, Florida, 23-25 October 1990.
5. Meijer, J. J. and Cunningham, A. M., Jr.., “Understanding and Development of a Prediction Method for Transonic Limit Cycle Oscillation Characteristics of Fighter Aircraft”, AIAA Paper No. 92-4501, August 1992.
6. Meijer, J. J. and Cunningham, A.M., Jr.., “A Semi-Empirical Non-Linear Aerodynamic Model to Predict Transonic LCO Characteristics of Fighter Aircraft”, AIAA Paper No. 95-1340, April 1995.
7. Cunningham, A. M Jr., “Non-Linear Aeroelastic Problems and Their Impact on Structural Integrity”, Proceedings Air Force 4r Aging Aircraft Conference, 9-11 July, 1996. th
8. Cunningham, A. M., Jr.., A Generic Non- Linear Aeroelastic Method with Semi- Empirical Non-Linear Unsteady Aerodvnamics. to be published as a Wright Laboratory Report, 1998.
9. Dobbs, S. K., Miller, G. D., and Stevenson, J. R., “Self Induced Oscillation Wind Tunnel Test of a Variable Sweep Wing”, AIAA Paper No. 85-0739-CP.
10. Cunningham, A. M., Jr.., “Aerodynamic Aspects of Transonic Limit Cycle Oscillations”, Aeroelasticitv and Fluid Structure Interaction Problems. ASME Publication AD - Vol 44, 1994.
11. Elbers, W.K., Wind Tunnel Data Report 1/9- Scale F-16A Pressure Model Investigation of Shock-Induced Separation for Limit Cycle Oscillation Studies (AEDC PWT-16T Test TF-695). General Dynamics, Fort Worth Division Report 16PR4694, September 1985.
12. Rudin, S.A., Analysis of F-16/LANTIRN Turbulence Test Results. Test TF-672. General Dynamics, Fort Worth Division Report 16PR4692, February 1985.