Article ID Journal Published Year Pages File Type
4911980 Composite Structures 2017 41 Pages PDF
Abstract
Thus, it is possible to utilize the load bearing capability of launch-vehicle primary structures up to 40% more effectively, resulting in considerable weight saving potentials for composite shell structures.
Keywords
Related Topics
Physical Sciences and Engineering Engineering Civil and Structural Engineering
Preview
Robust knockdown factors for the design of axially loaded cylindrical and conical composite shells - Development and Validation
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