Dynamic Response of Aluminum Honeycomb Panels to High-Frequency Laser Shock Excitations
Author:
Affiliation:
1. Yantai University, 264005 Yantai, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Reference12 articles.
1. Mathematical Model for the Separation Behavior of Low-Shock Separation Bolts
2. Hypervelocity Impact Testing of Multiwall Targets Using Multiple Simultaneously Launched Projectiles
3. Mechanical response of metallic honeycomb sandwich panel structures to high-intensity dynamic loading
4. Dynamic response and residual stress fields of Ti6Al4V alloy under shock wave induced by laser shock peening
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