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Development of a Design Methodology for Ducted Fan Systems Used in Micro Unmanned Air Vehicle Propulsion

[+] Author Affiliations
Abraham Engeda

Michigan State University, East Lansing, MI

Paper No. GT2006-91026, pp. 429-438; 10 pages
doi:10.1115/GT2006-91026
From:
  • ASME Turbo Expo 2006: Power for Land, Sea, and Air
  • Volume 5: Marine; Microturbines and Small Turbomachinery; Oil and Gas Applications; Structures and Dynamics, Parts A and B
  • Barcelona, Spain, May 8–11, 2006
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 0-7918-4240-1 | eISBN: 0-7918-3774-2
  • Copyright © 2006 by ASME

abstract

This paper presents an aerodynamic loss prediction and design methodology that has been developed for ducted-fan system of a vertical takeoff and landing Micro Unmanned Air Vehicle (Micro UAV). The method is based on a parametric geometry model and semi-empirical aerodynamic methods. The developed loss correlation method was applied to an initial sizing attempt of a ducted fan system.

Copyright © 2006 by ASME

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