Construction of Compressible Euler Solver Using Building-Cube Method and Application to Flutter Analysis of Aircraft Wing-Reference-Cited by-同舟云学术

Construction of Compressible Euler Solver Using Building-Cube Method and Application to Flutter Analysis of Aircraft Wing

Published:2014 Issue:2 Volume:62 Page:39-46
ISSN:1344-6460
Container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Author:

NISHIMURA Yasutaka,SASAKI Daisuke,NAKAHASHI Kazuhiro

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/jjsass/62/2/62_62_39/_pdf

Reference20 articles.

1. 2) Nakahashi, K., Ito, Y. and Togashi, F.: Some Challenges of Realistic Flow Simulations by Unstructured Grid CFD, Int. J. Numer. Methods Fluids, 43 (2003), pp. 769-783.

2. 3) Takenaka, K., Hatanaka, K., Yamazaki, W. and Nakahashi, K.: Multi-Disciplinary Design Exploration for Winglet, J. Aircraft, 45 (2008), pp. 1601-1611.

3. 4) Nakahashi, K. and Kim, L. S.: Building-Cube Method for Large-Scale, High Resolution Flow Computations, AIAA Paper 2004-0423, 2004.

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