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Daniel Guggenheim School of Aerospace Engineering
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Implementation of a Technology Impact Forecast Technique on a Civil Tiltrotor
A Comparative Assessment of Highspeed Rotorcraft Concepts (HSRC) : Reaction Driven Stopped Rotor/Wing and Variable Diameter Tiltrotor
An Assessment of Reaction Driven Stopped Rotor/Wing Using Circulation Control in Forward Flight
Technology for Rotorcraft Affordability Through Integrated Product/Process Development (IPPD)
Generating Dynamic Models Including Uncertainty for Use in Aircraft Conceptual Design
Development of a Methodology for the Determination of Technical Feasibility and Viability of Affordable Rotorcraft Systems
IPPD Through Robust Design Simulation for an Affordable Short Haul Civil Tiltrotor