Finite element engine blade structural optimization
- 15 April 1985
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Structural tailoring of engine blades (STAEBL)Published by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- A simple quadrilateral shell elementComputers & Structures, 1978
- Pseudo-Static Deformation and Frequencies of Rotating Turbomachinery BladesAIAA Journal, 1972
- Reduction of stiffness and mass matricesAIAA Journal, 1965