The objective of this research is to develop optimization procedures to provide design trends in high speed prop-rotors. The necessary disciplinary couplings are all considered within a closed loop optimization process. The procedures involve the consideration of blade aeroelastic, aerodynamic performance, structural and dynamic design requirements. Further, since the design involves consideration of several different objectives, multiobjective function formulation techniques are developed.
Optimum Design of High Speed Prop-Rotors
1992-10-12
Report
No indication
English
Optimum Design of High-Speed Prop-Rotors
NTRS | 1993
|Optimum Design of High-Speed Prop-Rotors
NTIS | 1993
|Optimum Design of High Speed Prop-Rotors
NTIS | 1992
|Optimization Procedure for Design of High-Speed Prop-Rotors
Online Contents | 1994
|