Limit cycle behavior of an airfoil with a control surface

Journal of Fluids and Structures

Volumn 12, Issue 7, 1998, Pages 839-858

  Tang, D ^a   Dowell, E H ^a   Virgin, L N ^a  

^a Duke University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0000969084     PISSN: 08899746     EISSN: None     Source Type: Journal    
DOI: 10.1006/jfls.1998.0174     Document Type: Article

References (5)

1. CONNER, M. D., TANG, D. M., DOWELL, E. H. & VIRGIN, L. N. 1997 Nonlinear behavior of a typical airfoil section with control surface freeplay: a numerical and experimental study. Journal of Fluids and Structures, 11, 89-109.
2. PETERS, D. A. & CAO, W. M. 1995 Finite state induced flow models; part I: two-dimensional thin airfoil. Journal of Aircraft 32, 313-322.
3. TANG, D. M., CONNER, M. C. & DOWELL, E. H. 1998 Reduced order finite-state airloads and its applications to a nonlinear aeroelastic system. Journal of Aircraft, 35, 332-338.
4. HSU, J. C. & MEYER, A. V. 1968 Modern Control Principles and Application, Chapter 6. New York: McGraw-Hill.
5. LACABANNE, M. & HUMBERT, M. 1997 An experimental analysis of the aeroelastic behavior with a freeplay in a control surface. Proceedings of the International Forum on Aeroelasticity and Structural Dynamics (ed. L. Morino, 17-20 June, Rome, Italy, pp. 239-246.