1 |
Conner, M. D., Tang, D. M., Dowell, E. H., and Virgin, L. N., 'Nonlinear Behavior of a Typical Airfoil Section with Control Surface Freeplay : A Numerical and Experimental Study', Journal of Fluidand Structures, Vol. 11, 1997, pp. 89-109
DOI
ScienceOn
|
2 |
Lee, I. and Kim, S. H., 'Aeroelastic Analysis of a Flexile Control Surface with Structural Nonlinearity', Journal of Aircraft, Vol. 32, No.4, 1995, pp. 868-874
DOI
ScienceOn
|
3 |
Bae, J. S. and Lee, I., 'Limit Cycle Oscillation of Missile Control Fin with Structural Nonlinearity', Journal of Sound and Vibration, Vol.269, No. 3-5, 2004, pp.669-687
DOI
ScienceOn
|
4 |
Bae, J.S., Kim, D.K., Shin, W.H., Lee, I., and Kim, S.H., 'Nonlinear Aeroelastic Analysis of a Deployable Missile Control Fin', Journal of Spacecraft and Rockets, Vol. 41, 2004
|
5 |
Ueda, T. and Dowell, E. H., 'A New Solution Method for Lifting Surfaces in Subsonic Flow', AIAA Journal, Vol. 20, No.3, 1982, pp. 348-355
DOI
ScienceOn
|
6 |
Shen, S. F 'An Approximate Analysis of Nonlinear Flutter Programs', Journal of Aerospace Science, Vol. 28, Jan. 1959, pp. 25-32
|
7 |
Woolston, D. S., Runyan, H. W., and Andrews, R. E., 'An Investigation of Effects of Certain Type of Structural Nonlinearities on Wing and Control Surface Flutter', Journal of Aeronautical Sciences, Vol. 24, Jan. 1957, pp. 57-63
DOI
|
8 |
Laurenson, R. M., and Trn, R. M., 'Flutter Analysis of Missile Control Surface Containing Structural Nonlinearities', AIAA Journal, Vol. 18, No. 10, 1980, pp. 1245-1251
DOI
ScienceOn
|
9 |
Lee, C. L., 'An Iterative Procedure for Nonlinear Flutter Analysis', AIAA Journal, Vol. 24, No.5, 1986, pp. 833-840
DOI
ScienceOn
|
10 |
Potkanski, W., 'Flutter Analysis of a System with Interacting Nonlinearities', Proceedings of the Eureopean Form on Aeroelasiticity and Structural Dynamics, 1991, pp. 315-318
|
11 |
Yang, Z. C. and Zhao, L. C, 'Analysis of Limit Cycle Flutter of an Airfoil in Incompressible Flow', Journal of Sound and Vibration, Vol. 123, No. 1,1988, pp.1-13
DOI
ScienceOn
|
12 |
Press, W. H., Flanner, B. P., Teukolsky, S. A., and Vetterling, W. T., Numerical Recipes: The art of scientific computation, Cambridge University Press, 1986
|
13 |
Brase, L. O. and Eversman W., 'Application of Transient Aerodynamics to Structural Nonlinear Flutter Problem', Journal of Aircraft, Vol. 25, No. 11, 1988, pp. 1060-1068
DOI
ScienceOn
|
14 |
Karpel, M., 'Design for Active Flutter Suppression and Gust Alleviation using State-space Aeroelastic Modeling', Journal of Aircraft, Vol. 19, No.3, 1982, pp. 221-227
DOI
ScienceOn
|
15 |
Bae, J. S., Aeroelastic Characteristics and Flutter Suppression considering Structural Nonlinearity, Ph.D Dissertation, Department of Aerospace Engineering, Korea Advanced Institute of Science Technology, 2002
|
16 |
Gelb, A. and Vander Velde, W. E., Multiple-Input Describing Functions and Nonlinear System Design,McGraw-Hill, New York, 1986
|
17 |
배재성, 신원호, 이인, 선영석, '이선형 비선형성을 포함하는 접는 미사일 조종날개의 공탄성 해석', 한국항공우주학회 지, 제 30권, 제 7호, pp.29-35, 2002
|
18 |
배재성, 김종윤, 양승만, 이인, '평판 날개의 아음속 플러터 실험 및 해석', 한국항공우주학회지, 제 30권, 제 5호, pp.56-61, 2002
|