Finite element analysis of F-16 aircraft canopy dynamic response to bird impact loading
- 12 May 1980
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Characterization of Bird Impacts on a Rigid Plate: Part 1Published by Defense Technical Information Center (DTIC) ,1975