Investigation of limit cycle oscillations for a wing section with nonlinear stiffness

Aerospace Science and Technology

Volumn 8, Issue 1, 2004, Pages 27-34

  Berggren, Daniel ^a  

^a ROYAL INSTITUTE OF TECHNOLOGY   (Sweden)

Author keywords

Aeroelasticity; Nonlinear; Structural dynamics; Unsteady aerodynamics

Indexed keywords

EIGENVALUES AND EIGENFUNCTIONS; MATHEMATICAL MODELS; NONLINEAR SYSTEMS; OSCILLATIONS; ROTATION; UNSTEADY FLOW; VECTORS; WIND TUNNELS; WINGS;

MASS MATRICES; NONLINEAR MOMENTUM;

AERODYNAMICS;

EID: 0347603505     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2003.08.006     Document Type: Article

References (13)

1. Bisplinghoff R.L., Ashley H., Halfman R.L. Aeroelasticity. 1957;Addison-Wesley, Reading, MA.
2. Barlow J., Rae W., Pope A. Low Speed Wind Tunnel Testing. 1999;Wiley, New York.
3. Castro B.M., Ekaterinaris J.A., Platzer M.F. Navier-Stokes analysis of wind-tunnel interference on transonic airfoil flutter. AIAA J. 40:(7):2002;1269-1276.
4. P.C. Chen, D. Sarhaddi, D.D. Liu, Limit-cycle oscillation studies of a fighter with external stores, AIAA Paper 98-1727, 1998, pp. 258-266.
5. Denegri C. Limit cycle oscillation flight test results of a fighter with external stores. J. Aircraft. 37:(5):2000;761-769.
6. Kuttenkeuler J. Optical measurements of flutter mode shapes. J. Aircraft. 37:(5):2000;846-849.
7. Norton W.J. Limit cycle oscillations and flight flutter testing. Proceedings of the 21st Annual Symposium, Society of Flight Test Engineers, Lancaster, CA. 1990;3.4.1-3.4.12.
8. Patil M.J., Hodges D.H., Cesnik C.E.S. Nonlinear aeroelastic analysis of complete aircraft in subsonic flow. J. Aircraft. 37:(5):2000;761-769.
9. Patil M.J., Hodges D.H., Cesnik C.E.S. Limit-cycle oscillations in high-aspect-ratio wings. J. Fluids and Structures. 15:(1):2001;107-132.
10. Patil M.J., Hodges D.H., Cesnik C.E.S. Nonlinear aeroelasticty and flight dynamics of high-altitude long-endurance aircraft. J. Aircraft. 38:(1):2001;88-94.
11. Peterson L.D., Crawley E.F. Improved exponential time series approximation of unsteady aerodynamic operators. J. Aircraft. 25:(2):1988;121-127.
12. Tang D., Dowell E., Kenneth C. Limit cycle oscillations of a cantilever wing in low subsonic flow. AIAA J. 37:(3):1999;364-371.
13. Tang D., Henry J., Dowell E. Limit cycle oscillations of delta wing models in low subsonic flow. AIAA J. 37:(11):1999;1355-1363.