Modeling limit cycle oscillations for an NLR 7301 airfoil aeroelastic configuration including correlation with experiment

44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Volumn , Issue , 2003, Pages

  Thomas, Jeffrey P ^a   Dowell, Earl H ^a   Hall, Kenneth C ^a  

^a Duke University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTIC CONFIGURATION; AEROELASTIC MODELING; FLUTTER ONSET; FREQUENCY DOMAINS; HARMONIC BALANCE; LIMIT CYCLE OSCILLATION (LCO); TRANSONIC AIRFOILS; WALL INTERFERENCE;

AIRFOILS; COMPUTATIONAL FLUID DYNAMICS; FIGHTER AIRCRAFT; STRUCTURAL DYNAMICS; WIND TUNNELS;

AEROELASTICITY;

EID: 84896859820     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

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2. Thomas, J. P., Dowell, E. II. Hall, K. C., "Nonlinear Inviscid Aerodynamic Effects on Transonic Divergence, Flutter and Limit Cycle Oscillations, " AIAA Journal, Vol. 40, No. 4, 2002, pp. 638-646.
3. Kholodar, D. B., Thomas, J. P., Dowell, E. II. Hall, K. C., "A Parameter Study of Transonic Airfoil Flutter on Limit Cycle Oscillation Behavior, " AIAA Paper 2001-1211, 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials (SDM) Conference, Denver, CO, April 2002.
4. Thomas. J. P., Dowell, E. II. Hall, K. C., "A Harmonic Balance Approach for Modeling Three-Dimensional Nonlinear Unsteady Aerodynamics and Aeroelasticity, " ASME Paper IMECE-2002-32532, Proceedings of the ASME International Mechanical Engineering Conference and Exposition, November 17-22, 2002, New Orleans, Louisiana, USA.
5. Thomas. J. P., Dowell, E. II. Hall, K. C., "Modeling Viscous Transonic Limit Cycle Oscillation Behavior Using a Harmonic Balance Approach, " AIAA Paper 2002-1414, 43th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials (SDM) Conference, Denver, CO, April 2002.
6. Schewe, G., Deyhle, H., "Experiments on Transonic Flutter of a Two-Dimensional Supercritical Wing with Emphasis on Non-Linear Effects, " Proceeding of the Royal Aeronautical Society Conference on Unsteady Aerodynamics, London, UK, July 17-18, 1996.
7. Scliowc. G., Knipfer, A., Mai, II. Dietz, G., "Experimental and Numerical Investigation of Nonlinear Effects in Transonic Flutter, " English Version (Translated by Dr. W. F. King III), German Aerospace Center DLR Final Report Number DLR IB 232-2002 J 01, Corresponds to Final Report for BMBF: Nichtlineare Effekte beim transsonischen Flattern (FKZ 13 N 7172), and Internal Report DLR IB 2001 J03, January 25, 2002.
8. 3, " AIAA Paper 98-0653, 36th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 1998.
9. Weber, S., Jones, K. D., Ekaterinaris, J. A., Platzer, M. F., "Transonic Flutter Computations for a 2D Supercritical Wing, " AIAA Paper 99-0798, 36th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 1999.
10. Tang, L., Bartels, R. E., Chen, P. C., Liu, D. I. "Simulation of Transonic Limit Cycle Oscillations Using a CFD Time-Marching Method, " AIAA Paper 2001-1290, 42th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials (SDM) Conference, Seattle, WA, April 2001.
11. Castro. B. M., Ekaterinaris, J. A., Platzer, M. F., "Navier-Stokes Analysis of Wind-Tunnel Interference on Transonic Airfoil Flutter, " AIAA Journal, Vol. 40, No. 7, 2002, pp. 1269-1276.