Generalized Sizing Methodology for Hybrid Aircraft Using Integrated Performance Constraints
Author:
Affiliation:
1. University of Calgary, Calgary, Alberta T2N 1N4, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference34 articles.
1. AlliP. “Erica: The European Tiltrotor. Design and Critical Technology Projects,” AIAA Paper 2003-2515, July 2003. doi:10.2514/6.2003-2515
2. A survey of hybrid Unmanned Aerial Vehicles
3. Simulation and analysis of V-22 tiltrotor aircraft forward-flight flowfield
4. CFD calculations on the unsteady aerodynamic characteristics of a tilt-rotor in a conversion mode
5. Numerical study on flow fields and aerodynamics of tilt rotor aircraft in conversion mode based on embedded grid and actuator model
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