Further investigation of modeling limit cycle oscillation behavior of the F-16 fighter using a harmonic balance approach

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

Volumn 3, Issue , 2005, Pages 1457-1466

  Thomas, Jeffrey P ^a,c,d   Dowell, Earl H ^a,d,e   Hall, Kenneth C ^a,c,d   Denegri Jr , Charles M ^b,d,f  

^a DUKE UNIVERSITY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c Department of Mechanical Engineering and Materials Science ^*  (United States)

^d AIAA   (United States)

^e School of Engineering

^f Certification Division

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTIC DEFORMATION; FIGHTER CONFIGURATION; LIMIT CYCLE; WINGTIP GEOMETRY;

AERODYNAMICS; COMPUTER SIMULATION; FIGHTER AIRCRAFT; FLUTTER (AERODYNAMICS); FREQUENCY DOMAIN ANALYSIS; HARMONIC ANALYSIS; WINGS;

OSCILLATIONS;

EID: 28844475166     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. Thomas, J. P., Dowell, E. H., and Hall, K. C., "Modeling Limit Cycle Oscillation Behavior of the F-16 Fighter Using a Harmonic Balance Approach," AIAA Paper 2004-1696, Presented at the 45th AIAA/ASME/ASCE/AHS/ ASC Structures, Structural Dynamics and Materials (SDM) Conference, Palm Springs, CA.
2. Hall, K. C., Thomas, J. P., and Clark, W. S., "Computation of Unsteady Nonlinear Flows in Cascades Using a Harmonic Balance Technique," AIAA Journal, Vol. 40, No. 5, May 2002, pp. 879-886.
3. Thomas, J. P., Dowell, E. H., and Hall, K. C., "Nonlinear Inviscid Aerodynamic Effects on Transonic Divergence, Flutter and Limit Cycle Oscillations," AIAA Journal, Vol. 40, No. 4, April 2002, pp. 638-646.
4. Thomas, J. P., Dowell, E. H., and Hall, K. C., "Modeling Viscous Transonic Limit Cycle Oscillation Behavior Using a Harmonic Balance Approach," AIAA Paper 2002-1414.
5. Thomas, J. P., Dowell, E. H., and Hall, K. C., "A Harmonic Balance Approach for Modeling Three-Dimensional Non-linear Unsteady Aerodynamics and Aeroelasticity," ASME Paper IMECE-2002-32532.
6. Thomas, J. P., Hall, K. C., and Dowell, E. H., "A Harmonic Balance Approach for Modeling Nonlinear Aeroelastic Behavior of Wings in Transonic Viscous Flow," AIAA Paper 2003-1924.
7. Charles M. Denegri, J. and Dubben, J. A., "In-Flight Wing Deformation Characteristics During Limit Cycle Oscillations," AIAA Paper 2003-1426.
8. Ni, R.-H., "A Multiple Grid Scheme for Solving the Euler Equations," AIAA Journal, Vol. 20, No. 11, November 1982, pp. 1565-1571.
9. Davis, R. L., Ni, R. H., and Bowley, W. W., "Prediction of Compressible, Laminar Viscous Flows Using a Time-Marching Control Volume and Multiple-Grid Technique," AIAA Journal, Vol. 22, No. 11, November 1984, pp. 1573-1581.
10. Saxor, A. P., "A Numerical Analysis of 3-D Inviscid Stator/Rotor Interactions Using Non-Reflecting Boundary Conditions," Tech. Rep. 209, MIT, March 1992, Gas Turbine Laboratory Report 209.
11. Spalart, P. R. and Allmaras, S. R., "A One Equation Turbulence Model for Aerodynamic Flows," AIAA Paper 92-0439.