Fluid-structural design analysis for composite aircraft wings with various fiber properties-Reference-Cited by-同舟云学术

Fluid-structural design analysis for composite aircraft wings with various fiber properties

Published:2021 Issue:1 Volume:16 Page:JFST0009-JFST0009
ISSN:1880-5558
Container-title:Journal of Fluid Science and Technology
language:en
Short-container-title:JFST

Author:

DATE Shugo¹²,ABE Yoshiaki²,YAMAMOTO Takeki¹,OKABE Tomonaga¹³

Affiliation:

1. Department of Aerospace Engineering, Tohoku University

2. Institute of Fluid Science, Tohoku University

3. Department of Materials Science and Engineering, University of Washington

Publisher

Japan Society of Mechanical Engineers

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering

Link

https://www.jstage.jst.go.jp/article/jfst/16/1/16_2021jfst0009/_pdf

Reference37 articles.

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2. Baker, A. A., and Scott, M., L., Composite Materials for Aircraft Structures (2004), p. 2, 87, AIAA Education Series, American Institute of Aeronautics and Astronautics.

3. Bathe, K., J., Finite element procedures (2006), Klaus-Jurgen Bathe.

4. Bram, V., T., Towards the Ultimate Conservative Difference Scheme. V. A Second-Order Sequel to Godounov's Method, Journal of Computational Physics, Vol. 32, (1979), pp. 101-136.

5. Christensen, R., M., Stress based yield/failure criteria for fiber composites, International Journal of Solids and Structures, Vol. 34, (1997), pp. 529-543.

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