Inverse design method for wings of supersonic transport

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

研究成果: Paper査読

5 被引用数 (Scopus)

抄録

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.

本文言語English
DOI
出版ステータスPublished - 1998
イベント36th AIAA Aerospace Sciences Meeting and Exhibit, 1998 - Reno, United States
継続期間: 1998 1 121998 1 15

Other

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

ASJC Scopus subject areas

  • 工学(全般)
  • 宇宙惑星科学

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