Inverse design method for wings of supersonic transport

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Jeong, Shinkyu ^a,d   Matsushima, Kisa ^b,e   Iwamiya, Toshiyuki ^c,f   Obayashi, Shigeru ^a   Nakahashi, Kazuhiro ^a,d  

^a TOHOKU UNIVERSITY   (Japan)

^b FUJITSU LABORATORIES LTD   (Japan)

^c JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^d Dept of Aeronautics and Space Engineering ^*

^e Supercomputer Systems Engineering Division

^f Computer Science Division ^*

Author keywords

[No Author keywords available]

Indexed keywords

INVERSE PROBLEMS; ITERATIVE METHODS; SUPERSONIC AIRCRAFT; TRANSPORT AIRCRAFT; WINGS;

INVERSE DESIGN METHODS; POINT OF INTEREST; RESIDUAL CORRECTION; SMALL PERTURBATIONS; SUPERSONIC TRANSPORT;

DESIGN;

EID: 84983127088     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-602     Document Type: Conference Paper

References (10)

1. Carlson, H. W. and Miller, D. S., "Numerical Methods for the Design and Analysis of Wings at Supersonic Speed," NASA TN D-7713, 1974.
2. Yoshida, K. and Hayama, K., "Experimental and Numerical Study of Aerodynamic Characteristics for Second generation SST," SAE paper 91-2056, 1991.
3. K. B. Walkley, and G. E. Smith, "Application of a Full Potential Method to Supersonic Aircraft Design and Analysis," Journal of Aircraft, Vol. 26, No. 1, pp. 6-12, Jan., 1989.
4. Kamiya, N., Tamaki, H., Hirose, N., and Ishida Y., "On an Inverse Problem for a Supersonic Airfoils Based on Navier-Stokes Approximation," Proc. of 14th the NAL Symposium on Aircraft Computational Aerodynamic, 1997 (in Japanese).
5. Takanashi, S., "Iterative Three-Dimensional Transonic Wing Design Using Integral Equations, " Journal of Aircraft, Vol. 22, No. 8, pp. 655-660, Aug. 1985.
6. Heaslet, M. A., Lomax, H., and Jones, A. L., "Volterra's Solution of the Wave Equation as Applied to Three-Dimensional Supersonic Airfoil Problem," NACA Rep. 899, 1947. (Formerly NACA TN 1412.)
7. Lomax, H., Heaslet, M. A. and Franklyn, B. Fuller, "Integrals and Integral Equation in Linearized Wing Theory," NACA Rep. 1054, 1951.
8. Carlson, H. W. and Middleton, W. D., "A Numerical Method for Design of Camber Surfaces of Supersonic Wings with Arbitrary Planforms," NASA TN-2341, 1964.
9. Obayashi, S. and Guruswamy, G. P., "Navier-Stokes Computations for Oscillating Control Surface, " Journal of Aircraft, Vol. 31, No. 3, pp. 631-636, May-June, 1994.
10. Obayashi, S., Jeong, S. and Matsuo, Y., "New Blunt Trailing-Edge Airfoil Designed by Inverse Optimization Method," Journal of Aircraft, Vol. 34, No. 2, pp. 255-257, March-April, 1997.