Optimum design of high speed prop-rotors using a multidisciplinary approach

Optimum design of high speed prop-rotors using a multidisciplinary approach

0.00 Avg rating0 Votes
Article ID: iaor19941489
Country: Switzerland
Volume: 22
Issue: 1
Start Page Number: 1
End Page Number: 17
Publication Date: Nov 1993
Journal: Engineering Optimization
Authors: ,
Keywords: design, optimization
Abstract:

The design of advanced high speed prop-rotor aircraft is addressed using a formal multidisciplinary optimization procedure. The optimization problem is formulated with aerodynamic performance, dynamics, aeroelastic stability and structural design requirements. Both high speed cruise and hover flight conditions are addressed. The analysis is performed at a cruise speed of 400 knots. The efficiency in cruise is maximized without deteriorating hover performance. Constraints are imposed on fundamental frequency, blade weight, thrust in hover, total power required and aeroelastic stability in cruise. A wide selection of structural and aerodynamic design varaibles are used. The optimization is performed using a nonlinear programming procedure and an approximate analysis technique. The procedure yields significant improvements in the overall rotor performance.

Reviews

Required fields are marked *. Your email address will not be published.