Improper integrals in the formulation of a supersonic inverse problem-Reference-Cited by-同舟云学术

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Improper integrals in the formulation of a supersonic inverse problem

Published:2000 Issue: Volume: Page:399-407
ISSN:
Container-title:Inverse Problems in Engineering Mechanics II
language:
Short-container-title:

Author:

Matsushima Kisa

Publisher

Elsevier

Reference6 articles.

1. Iterative Three-Dimensional Transonic Wing Design Using Integral Equations;Takanashi;J. Aircraft,1985

2. Aerodynamic Wing Design for NAL's SST Using an Iterative Inverse Approach;Matsushima,1998

3. Supersonic Inverse Design Method and Its Application to Japanese SST;Matsushima,1999

4. Aerodynamic Design of Supersonic Experimental Airplane;Iwamiya,2000

5. Integrals and Integral Equations in Linearized Wing Theory;Lomax;NACA Rep.,1951

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Aerodynamic Wing Design of NEXST-2 Using Unstructured-Mesh and Supersonic Inverse Problem;Journal of Aircraft;2004-09

2. Aerodynamic shape design of laminar wings for Japanese experimental SST;40th AIAA Aerospace Sciences Meeting & Exhibit;2002-01-14

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