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Introduction
Attempt at a Very Early Preliminary Design of an Optimal Composite Rotor Blade for the V-22 Osprey
Carl Banks
1
The Pennsylvania State University
University Park, Pennsylvania
Introduction
Design Requirements
Strength
Optimal Twist
Similarity to Current V-22 Design
Static Analysis
Blade Coordinate System
Beam Model
Discretization of the Blade
Blade Loading in Hover
Failure Analysis
Design Methodology
Results
Conclusion
Bibliography
Appendix
About this document ...
Next:
Introduction
Carl Banks
2000-05-04
