Organizational Unit:
Daniel Guggenheim School of Aerospace Engineering
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Implementation of a Technology Impact Forecast Technique on a Civil Tiltrotor
Generating Dynamic Models Including Uncertainty for Use in Aircraft Conceptual Design
Reduced Order Guidance Methods and Probabilistic Techniques in Addressing Mission Uncertainty
Application of Probabilistic Methods for the Determination of an Economically Robust HSCT Configuration
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
System Synthesis in Preliminary Aircraft Design Using Statistical Methods
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
A New Approach to Integrated Wing Design in Conceptual Synthesis and Optimization
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