Integrated determination of sensitivity derivatives for an aeroelastic transonic wing

Journal of Aircraft

Volumn 33, Issue 1, 1996, Pages 224-231

  Arslan, Alan E ^a,b   Carlson, Leland A ^a,b  

^a Texas AandM University   (United States)

^b AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; ITERATIVE METHODS; MATHEMATICAL MODELS; OPTIMIZATION; PRESSURE MEASUREMENT; SENSITIVITY ANALYSIS; TRANSONIC FLOW;

AERODYNAMIC SENSITIVITY; AEROELASTIC TRANSONIC WINGS; SENSITIVITY DERIVATIVES; TWISTED UNSWEPT RECTANGULAR WINGS;

WINGS;

EID: 0029716993     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/3.46925     Document Type: Article

References (12)

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8. Sobieszczanski-Sobieski, J., "Multidisciplinary Optimization for Engineering Systems: Achievements and Potential," NASA TM 101566, March 1989.
9. Arslan, A. E., "Analysis and Numerical Computation of Sensitivity Derivatives in the Transonic Regime," M.S. Thesis, Texas A&M Univ., College Station, TX, Dec. 1993.
10. Arslan, A. E., and Carlson, L. A., "Integrated Determination of Sensitivity Derivatives for an Aeroelastic Transonic Wing," AIAA Paper 94-4400, Sept. 1994.
11. Sobieszczanski-Sobieski, J., "Sensitivity of Complex Coupled Systems," AIAA Journal, Vol. 28, No. 1, 1990, pp. 153-160.
12. Weed, R. A., Anderson, W. K., and Carlson, L. A., "A Direct-Inverse Three Dimensional Transonic Wing Design Method for Vector Computers," AIAA Paper 84-2156, Aug. 1984.