Inverse design method for wings of supersonic transport

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

doi:10.2514/6.1998-602

Inverse design method for wings of supersonic transport

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

Creative Flow Research Division

Research output: Contribution to conference › Paper › peer-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 language	English
DOIs	https://doi.org/10.2514/6.1998-602
Publication status	Published - 1998
Event	36th AIAA Aerospace Sciences Meeting and Exhibit, 1998 - Reno, United States Duration: 1998 Jan 12 → 1998 Jan 15

Other

Other	36th AIAA Aerospace Sciences Meeting and Exhibit, 1998
Country/Territory	United States
City	Reno
Period	98/1/12 → 98/1/15

ASJC Scopus subject areas

Engineering(all)
Space and Planetary Science

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10.2514/6.1998-602

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title = "Inverse design method for wings of supersonic transport",

abstract = "A practical inverse design method for supersonic airfoils/wings has been developed. The method is based on Takanashi{\textquoteright}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.",

author = "Shinkyu Jeong and Kisa Matsushima and Toshiyuki Iwamiya and Shigeru Obayashi and Kazuhiro Nakahashi",

note = "Publisher Copyright: {\textcopyright} 1997, American Institute of Aeronautics and Astronautics, Inc.; 36th AIAA Aerospace Sciences Meeting and Exhibit, 1998 ; Conference date: 12-01-1998 Through 15-01-1998",

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doi = "10.2514/6.1998-602",

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TY - CONF

T1 - Inverse design method for wings of supersonic transport

AU - Jeong, Shinkyu

AU - Matsushima, Kisa

AU - Iwamiya, Toshiyuki

AU - Obayashi, Shigeru

AU - Nakahashi, Kazuhiro

PY - 1998

Y1 - 1998

N2 - 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.

AB - 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.

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DO - 10.2514/6.1998-602

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T2 - 36th AIAA Aerospace Sciences Meeting and Exhibit, 1998

Y2 - 12 January 1998 through 15 January 1998

ER -

Inverse design method for wings of supersonic transport

Abstract

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ASJC Scopus subject areas

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