Divergence speed degradation of forward-swept wings with damaged composite skin-Reference-Cited by-同舟云学术

Divergence speed degradation of forward-swept wings with damaged composite skin

Published:1984-11 Issue:11 Volume:21 Page:921-923
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Eastep F. E.¹,Venkayya V. B.²,Tishler V. A.²

Affiliation:

1. University of Dayton, Dayton, Ohio

2. AFWAL, Wright-Patterson Air Force Base, Ohio

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.45063

Reference10 articles.

1. Diederich, F W and Budiensky, B , Divergence of Swept Wings' NACATN1680 1948

2. On the Track of Practical Forward Swept Wings Astronautics and Aeronautics, Vol20Jan 1982pp4052

3. 5Starnes J H Jr and Haftka, R T. Preliminary Design of Composite Wing Box Structures for Global Damage Tolerance Proceedings of the 21st AIAA Structures Structural Dynamics and Materials Conference Seattle Wash , May 1980pp529538

4. Arora, J S Harg E S and Haskele D F Optimal Design if Damage Tolerant Structures ' Proceedings of the 2nd Symposium on Vulnerability and Survivability Vol I Washington D C Oct 1976pp.127132

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