Aerothermoelastic Stability of Composite Aerovehicle Wings Subjected to Heat Inputs
Author:
Affiliation:
1. Universit of Rome “La Sapienza”, 00184 Rome, Italy
2. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061-0219
3. Avio Propulsione Aerospaziale, 00034 Colleferro, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.32397
Reference32 articles.
1. Aeroelastic analysis of hypersonic vehicles
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3. Aerothermoelastic Response of a Functionally-Graded Aircraft Wing to Heat Loads;49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <br> 16th AIAA/ASME/AHS Adaptive Structures Conference<br> 10t;2008-04-07
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