Design and Manufacturing of Tow-Steered Composite Shells Using Fiber Placement
Author:
Affiliation:
1. NASA Langley Research Center
2. Adoptech, Inc.
3. NASA Marshall Space Flight Center
4. Lockheed Martin Corporation
5. U.S. Army Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-2700
Reference22 articles.
1. In-plane response of laminates with spatially varying fiber orientations - Variable stiffness concept
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