Wing design for supersonic transports using integral equation method-Reference-Cited by-同舟云学术

Wing design for supersonic transports using integral equation method

Published:2004-03 Issue:3 Volume:28 Page:247-255
ISSN:0955-7997
Container-title:Engineering Analysis with Boundary Elements
language:en
Short-container-title:Engineering Analysis with Boundary Elements

Author:

Matsushima Kisa,Iwamiya Toshiyuki,Nakahashi Kazuhiro

Publisher

Elsevier BV

Subject

Applied Mathematics,Computational Mathematics,General Engineering,Analysis

Reference10 articles.

1. Sakata K. Supersonic experimental airplane program in NAL and its CFD-design research demand, NAL's 2nd SST–CFD Workshop; 2000. p. 53–6.

2. Sakata K. Supersonic experimental airplane (NEXST) for next generation SST technology, AIAA-paper 2002-0527; 2002.

3. Shimbo Y, Yoshida K, Iwamiya T, Takaki R, Matsushima K. Aerodynamic design of scaled supersonic experimental airplane, NAL's 1st SST–CFD Workshop; 1998. p. 62–7.

4. Jeong S, Matsushima K, Iwamiya T, Obayashi S, Nakahashi K. Inverse design method for wings of supersonic transport, AIAA-paper 98-0602; 1998.

5. Improper integrals in the formulation of a supersonic inverse problem;Matsushima,2000

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