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- W912851519 abstract "A cyclocopter propelled by the cycloidal blade system, which can be described as a horizontal rotary wing, is a new concept of VTOL vehicle. In this paper, optimized structure design is carried out for the aerodynamically optimized cyclocopter rotor system. Database is obtained fer design variables such as stacking sequence (ply angles), number of plies and spar locations through MSC/NASTRAN and optimum values are determined by RSM and some other optimizing processes. For the rotor system including optimized blade and composite hub m, the maximum stress by static analysis is within the failure criteria. And the rotor system is designed for the purpose of avoiding possible dynamic instabilities by inconsistency between frequencies of rotor rotation and some low natural frequencies of rotor." @default.
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- W912851519 date "2005-01-01" @default.
- W912851519 modified "2023-09-24" @default.
- W912851519 title "Optimized Structure Design of Composite Cyclocopter Rotor System using RSM" @default.
- W912851519 hasPublicationYear "2005" @default.
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