File:Development of a cross-flow fan rotor for vertical take-off and landing aircraft (IA developmentofcro1094534703).pdf

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Original file(1,275 × 1,650 pixels, file size: 1.44 MB, MIME type: application/pdf, 74 pages)

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Development of a cross-flow fan rotor for vertical take-off and landing aircraft   (Wikidata search (Cirrus search) Wikidata query (SPARQL)  Create new Wikidata item based on this file)
Author
Martin, Michael J.
image of artwork listed in title parameter on this page
Title
Development of a cross-flow fan rotor for vertical take-off and landing aircraft
Publisher
Monterey, California: Naval Postgraduate School
Description

This study determined the optimum number of blades on a 4-inch diameter cross-flow fan rotor such that the rotor produced a thrust-to-weight ratio over one, which will make vertical take-off possible. The commercial computational fluid dynamics software ANSYS CFX, along with the commercial computer-aided design software SolidWorks, was used to model and perform a parametric study on the number of rotor blades. This parametric study focused on the thrust output, power requirement, and efficiency of each design in order to determine the optimum number of blades at 8,000 RPM. After the analytical study was complete, working models of three different rotors were fabricated and tested to validate the results found using ANSYS CFX. The experimental and analytical models were successfully compared at speeds ranging from 4,000 to 7,000 RPM.


Subjects: Vertical take-off; vertical take-off and landing (VTOL); cross-flow fan (CFF)
Language English
Publication date June 2013
Current location
IA Collections: navalpostgraduateschoollibrary; fedlink
Accession number
developmentofcro1094534703
Source
Internet Archive identifier: developmentofcro1094534703
https://archive.org/download/developmentofcro1094534703/developmentofcro1094534703.pdf
Permission
(Reusing this file)
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.

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Public domain
This work is in the public domain in the United States because it is a work prepared by an officer or employee of the United States Government as part of that person’s official duties under the terms of Title 17, Chapter 1, Section 105 of the US Code. Note: This only applies to original works of the Federal Government and not to the work of any individual U.S. state, territory, commonwealth, county, municipality, or any other subdivision. This template also does not apply to postage stamp designs published by the United States Postal Service since 1978. (See § 313.6(C)(1) of Compendium of U.S. Copyright Office Practices). It also does not apply to certain US coins; see The US Mint Terms of Use.

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Date/TimeThumbnailDimensionsUserComment
current09:08, 17 July 2020Thumbnail for version as of 09:08, 17 July 20201,275 × 1,650, 74 pages (1.44 MB) (talk | contribs)FEDLINK - United States Federal Collection developmentofcro1094534703 (User talk:Fæ/IA books#Fork8) (batch 1993-2020 #13783)

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