Nonlinear Responses of a Cantilever Wing with an External Store

Author:

Kim Kiun,Strganac Thomas

Publisher

American Institute of Aeronautics and Astronautics

Reference22 articles.

1. Limit Cycle Oscillation Characteristics of Fighter Aircraft

2. Limit Cycle Oscillation Flight Test Results of a Fighter with External Stores

3. Cycle Oscillation Studies of a Fighter with External Stores,"39thAIAA Structures, Structural Dynamics, and Materials Conference, AIAA Paper 98-1727, 1998. 4)Stearman, R.O., Powers, E.J., Schwartz, J., and

4. Yurkorvich, R. "Aeroelastic System Identification of Advanced Technology Aircraft Through Higher Order Signal Processing," inProceedings of the 9thInternational Modal Analysis Conference, Florence, Italy, April15-18,1991, pp.1607-1616. 5) Cole, S.R. "Effects of Spoiler Surfaces on the

5. Aeroelastic Behavior or a Low-Aspect ratio Wing" Proceedings ofthe 31stAIAA Structures, Structural Dynamics, and Materials Conference, AIAA Paper 90-0981, 1990, pp.1455-1463. 6)Oh, K., Nayfeh, A.H., and Mook, D.T. "Modal

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2. Nonlinear Responses of a Slender Wing With a Store;Journal of Vibration and Acoustics;2019-02-04

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4. Nonlinear aeroelastic analysis of high-aspect-ratio wings using indicial aerodynamics;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2018-05-19

5. Experimental investigation of linear and nonlinear aeroelastic behavior of a cropped delta wing with store in low subsonic flow;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2015-10-18

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