Interfacing of fluid and structural models via innovative structural boundary element method

AIAA Journal

Volumn 36, Issue 2, 1998, Pages 282-287

  Chen, P C ^a,b   Jadic, I ^a,c,d  

^a ZONA TECHNOLOGY INC   (United States)

^b Technical Staff ^*  (United States)

^c Technical Staff

^d Raytheon Aircraft Company   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0000137014     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.7513     Document Type: Article

References (12)

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8. 8Hounjet, M. H. L., and Meijer, J. J., "Evaluation of Elastomechanical and Aerodynamic Data Transfer Methods for Non-planar Configurations in Computational Aeroelastic Analysis," Proceedings of the International Forum on Aeroelasticity and Structural Dynamics (Manchester, England, UK), Royal Aeronautical Society, 1995, pp. 10.1-10.25.
9. 9Petiau, C., and Nicot, P., "A General Method for Mathematical Model Identification in Aeroelasticity," Proceedings of the International Forum on Aeroelasticity and Structural Dynamics, 1995, pp. 67.1-67.9.
10. 10Guruswamy, G. P., "Coupled Finite-Difference/Finite-Element Approach for Wing-Body Aeroelasticity," AIAA Paper 92-4680, 1992.
11. 11Batina, J. T., "Unsteady Euler Algorithm with Unstructured Dynamic Mesh for Complex-Aircraft Aeroelastic Analysis," AIAA Journal, Vol. 29, No. 3, 1991, pp. 327-333.
12. 12Brebbia, C. A., and Dominguez, J., Boundary Elements: An Introductory Course, McGnw-Hill, New York, 1992, Chap. 3.