Inverse design method for wings of supersonic transport

Shinkyu Jeong, Kisa Matsushima, Toshiyuki Iwamiya, Shigeru Obayashi, Kazuhiro Nakahashi

Research output: Contribution to conferencePaperpeer-review

5 Citations (Scopus)

Abstract

A practical inverse design method for supersonic airfoils/wings has been developed. The method is based on Takanashi’s iterative “residual-correction” concept. A geometry that materializes a specified pressure distribution is sought by solving an integrodifferential form of the linearized small perturbation (LSP) equation. The integration is limited to the Mach forecone from the point of interest. Several design results are presented.

Original languageEnglish
Publication statusPublished - 1998 Jan 1
Event36th AIAA Aerospace Sciences Meeting and Exhibit, 1998 - Reno, United States
Duration: 1998 Jan 121998 Jan 15

Other

Other36th AIAA Aerospace Sciences Meeting and Exhibit, 1998
CountryUnited States
CityReno
Period98/1/1298/1/15

ASJC Scopus subject areas

  • Engineering(all)
  • Space and Planetary Science

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