A model for predicting the behavior of impact-damaged minimum gage sandwich panels under compression
- 8 April 1991
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Design and Analysis of Composite Structures with Manufacturing FlawsJournal of the American Helicopter Society, 1990
- A correlation parameter for predicting the compressive strength of composite sandwich panels after low speed impactPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Analytical evaluations of damage of sandwich panelsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985