Soft Impact Damage Prognosis of F-16 Canopy Using Progressive Failure Dynamic Analysis-Reference-Cited by-同舟云学术

Soft Impact Damage Prognosis of F-16 Canopy Using Progressive Failure Dynamic Analysis

Published:2014-11 Issue:6 Volume:51 Page:1959-1965
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Siddens Aaron J.¹,Bayandor Javid¹,Abdi Frank²

Affiliation:

1. Crashworthiness for Aerospace Structures and Hybrids (CRASH) Lab, Department of Mechanical Engineering, Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061

2. AlphaSTAR Corporation, Long Beach, California 90804

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032937

Reference13 articles.

1. WilbeckJ. S. “Impact Behavior of Low Strength Projectiles,” U.S. Air Force Material Lab. TR-77-134, Wright Patterson AFB, OH, July 1978.

2. AbdiF. F.ClarkG. M. “High Performance Transparency Design,” Rockwell International, Los Angeles, CA, 1989.

3. Multidisciplinary impact damage prognosis methodology for hybrid structural propulsion systems

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