A Study of the Cantilevered Square Plate Subjected to a Uniform Loading
Author:
Affiliation:
1. North American Aviation, Inc.,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.9357
Reference13 articles.
1. Bending of a Uniformly Loaded Rectangular Plate With Two Adjacent Edges Clamped and the Others Either Simply Supported or Free
2. An Initial Approach to the Overall Structural Problems of Swept Wings Under Static Loads
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