Three dimensional nonlinear dynamic finite element analysis for the response of a thick laminated shell to impact loads
- 15 April 1985
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- MAGNA analysis of the T-38 aircraft student canopy - Response to in-flight aerodynamic pressure loadsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Simulation of T-38 aircraft student canopy response to cockpit pressure and thermal loads using MAGMAPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Finite element analysis of through the canopy emergency crew escape from the T-38 aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Finite element analysis of a bird-resistant monolithic stretched acrylic canopy design for the F-16A aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Finite element analysis of F-16 aircraft canopy dynamic response to bird impact loadingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980