Thermal Buckling Suppression of Supersonic Vehicle Surface Panels Using Shape Memory Alloy
Author:
Affiliation:
1. Old Dominion University, Norfolk, Virginia, 23529-0247
2. City University of Hong Kong, Kowloon, Hong Kong, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.5669
Reference25 articles.
1. Methodology for Supersonic Panel Flutter Analysis of Thermal Protection System Seals
2. A summary of recent research on the nitinol alloys and their potential application in ocean engineering
3. Experimental studies of structural acoustic control for a shape memory alloy composite beam
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