Integration of twenty-bladed cross-flow fan into vertical take-off and landing aircraft
Jones, Andria M.
Hobson, Garth V.
Gannon, Anthony J.
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The research presented is dedicated to determining an efficient rotor and housing system that will generate a sufficient thrust-to-weight ratio for vertical take-off and landing through computational modeling, implementation and experimentation. To accomplish this task, a new 20-bladed rotor was designed in SolidWorks and imported into ANSYS-CFX, which was used to analytically determine the thrust generated at speeds ranging from 4,000 rpm to 10,000 rpm. Upon successful simulation, a carbon-fiber model was fabricated and tested at speeds from 4,000 rpm to 9,700 rpm. With a promising thrust-to-weight ratio, a platform was built for initial testing utilizing two motors and four cross-flow fans. Initial platform testing was successful and generated sufficient thrust for vertical take-off.
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. As such, it is in the public domain, and under the provisions of Title 17, United States Code, Section 105, may not be copyrighted.
RightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
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