Finite element analysis of F-16 aircraft canopy dynamic response to bird impact loading-Reference-Cited by-同舟云学术

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Finite element analysis of F-16 aircraft canopy dynamic response to bird impact loading

Published:1980-05-12 Issue: Volume: Page:
ISSN:
Container-title:21st Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

MCCARTY R.¹

Affiliation:

1. USAF, Flight Dynamics Laboratory, Wright-Patterson AFB, Ohio

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1980-804

Reference23 articles.

Cited by 12 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

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3. Numerical Simulation of Bird Strike;Bird Strike in Aviation;2019-06-07

4. Finite element bird-strike modeling;Bird Strike;2016

5. Computational methods for bird strike simulations: A review;Computers & Structures;2011-12

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