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Daniel Guggenheim School of Aerospace Engineering
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A comparative study and application of continuously variable transmission to a single main rotor heavy lift helicopter
A new methodology for sizing and performance predictions of a rotary wing ejector
Design Methodology for Developing Concept Independent Rotorcraft Analysis and Design Software
Development and Implementation of Rotorcraft Preliminary Design Methodology using Multidisciplinary Design Optimization
A plm implementation for aerospace systems engineering-conceptual rotorcraft design
Composite skid landing gear design investigation
A Hybrid Optimization Scheme for Helicopters with Composite Rotor Blades
Optimal maintenance of a multi-unit system under dependencies
Optimal aeroelastic trim for rotorcraft with constrained, non-unique trim solutions
Preliminary Turboshaft Engine Design Methodology for Rotorcraft Applications