AN ENHANCED INTEGRATED AERODYNAMIC LOAD/DYNAMIC APPROACH TO OPTIMUM ROTOR BLADE DESIGN

An enhanced integrated aerodynamic load/dynamic optimization procedure is developed to minimize vibratory root shears and moments. The optimization problem is formulated with 4/rev vertical and 3/rev inplane shears at the blade root as objective functions and constraints are imposed on 3/rev radial shear, 3Aev flapping and torsional moments and 4/rev lagging moment. Constraints are also imposed on blade natural frequencies, weight, autorotational inertia, centrifugal stress and rotor thrust The ’Global Criteria Approach’ is used for formulating the multi-objective optimization. Design variables include spanwise distributions of blade bending stiffnesses, torsional stiffness, nonstructural mass, chord, radius of gyration and blade taper ratio. The program CAMRAD is coupled with an optimizer, which consists of the program CONMIN and an approximate analysis, to obtain optimum designs. The optimization procedure is applied to an advanced rotor as a reference design. Optimum blade designs, obtained with and without a constraint on the rotor thrust, are presented and are compared to the reference blade. Substantial reductions are obtained in the vibratory root forces and moments. As a byproduct, improvements are also found in some performance parameters, such as total power required, which were not considered during optimization.