Use of curvilinear fiber format in composite structure design
- 1 June 1991
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 29 (6) , 1011-1015
- https://doi.org/10.2514/3.10697
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Effect of bolt load proportioning on the capacity of multiple-bolt composite jointsJournal of Aircraft, 1988
- Importance of anisotropy on buckling of compression-loaded symmetriccomposite platesAIAA Journal, 1986
- Photoelastic determination of stresses in multiple-pin connectorsExperimental Mechanics, 1983
- Alleviation of the stress concentration with analogue reinforcementExperimental Mechanics, 1973
- Stress-Concentration Factors Around a Central Circular Hole in a Plate Loaded Through Pin in the HoleJournal of Applied Mechanics, 1940