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Volumn 3, Issue 3, 1988, Pages 233-260

Aerodynamic design via control theory

Author keywords

Computational aerodynamics; inverse problem; optimization; transonic flow; wing design

Indexed keywords


EID: 20544476549     PISSN: 08857474     EISSN: 15737691     Source Type: Journal    
DOI: 10.1007/BF01061285     Document Type: Article
Times cited : (1646)

References (21)
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    • Jameson, A., Schmidt, W., and Turkel, E. (1981). Numerical solution of the Euler equations by finite volume methods using Runge-Kutta time stepping schemes, AIAA Paper No. 81-1259, AIAA 14th Fluid Dynamics and Plasma Dynamics Conference, Palo, Alto, California.
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    • Jameson, A., Baker, T. J., and Weatherill, N. P. (1986). Calculation of inviscid transonic flow over a complete aircraft, AIAA Paper No. 86-0103, AIAA 24th Aerospace Sciences Meeting, Reno, Nevaca.
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    • McFadden, G. B. (1979). An artificial viscosity method for the design of supercritical airfoils, New York University report No. C00-3077-158.
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    • A multiple grid scheme for solving the Euler equations
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    • Ni, R.H.1
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    • Pulliam, T. H., and Steger, J. L. (1985). Recent improvements in efficiency, accuracy and convergence for implicit approximate factorization algorithms, AIAA Paper No. 85-0360, AIAA 23rd Aerospace Sciences Meeting, Reno, Nevada.
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    • Taverna, F. (1983). Advanced airfoil design for general aviation propellers, AIAA Paper No. 83-1791.
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.