A comprehensive and versatile analysis of the response of a helicopter rotor blade is presented in this paper. First, the full nonlinear partial differential equations that govern the motion of the blade, taking into account the geometrical nonlinearities that arise due to deformation, are presented
β¦ LIBER β¦
DROID analysis of the NASA helicopter images
β Scribed by Harris, Chris ;Stephens, Mike ;Sparks, Ed ;Pike, Mary
- Book ID
- 112186981
- Publisher
- John Wiley and Sons
- Year
- 1992
- Tongue
- English
- Weight
- 895 KB
- Volume
- 9
- Category
- Article
- ISSN
- 0741-2223
No coin nor oath required. For personal study only.
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