Thermal testing of tow-placed, variable stiffness panels
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
2. Virginia Polytechnic Inst. and State Univ., Blacksburg
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-1190
Reference12 articles.
1. In-plane response of laminates with spatially varying fiber orientations - Variable stiffness concept
2. BUCKLING RESPONSE OF LAMINATES WITH SPATIALLY VARYING FIBER ORIENTATIONS
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