An enhanced integrated aerodynamic load/dynamic optimization procedure for helicopter rotor blades, Volume 4326
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270 Azimuth angle 3/rev flapping 3/rev inplane shear 3/rev radial shear 3/rev torsional 4/rev lagging 4/rev vertical shear Aditi Chattopadhyay advancing blade Aerodynamic Load/Dynamic Optimization airfoil angle of attack attack with Mach autorotational inertia Azimuthal distributions blade airload blade model blade root blade weight centrifugal stress coefficient with Mach component of airload deg 360 Fig distributions of inplane Enhanced Integrated Aerodynamic forces and moments Helicopter Rotor inplane component Integrated Aerodynamic Load/Dynamic L/D)max Langley Research Center lb-ft lb/ft linear linear taper Load/Dynamic Optimization Procedure lower bound Mach number Fig move limit natural frequencies nonstructural weight normal component normalized local power number of blade objective functions optimization problem Optimum blade designs optimum design optimum rotor percent planform power coefficient program CAMRAD propulsive force radius of gyration Reference Optimum reference rotor root chord rotor thrust Services & Materials Taylor series thrust constraint tions Tref upper bound Variation of normalized