High speed bird impact analysis of the Learjet 45 windshield using DYNA3D
- 20 April 1998
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- 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