File:Integration of twenty-bladed cross-flow fan into vertical take-off and landing aircraft (IA integrationoftwe1094534682).pdf

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Original file(1,275 × 1,650 pixels, file size: 3.2 MB, MIME type: application/pdf, 90 pages)

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Integration of twenty-bladed cross-flow fan into vertical take-off and landing aircraft   (Wikidata search (Cirrus search) Wikidata query (SPARQL)  Create new Wikidata item based on this file)
Author
Jones, Andria M.
Title
Integration of twenty-bladed cross-flow fan into vertical take-off and landing aircraft
Publisher
Monterey, California: Naval Postgraduate School
Description

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.


Subjects: Vertical take-off; VTOL; cross-flow fan; CFF
Language English
Publication date June 2013
Current location
IA Collections: navalpostgraduateschoollibrary; fedlink
Accession number
integrationoftwe1094534682
Source
Internet Archive identifier: integrationoftwe1094534682
https://archive.org/download/integrationoftwe1094534682/integrationoftwe1094534682.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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current03:33, 22 July 2020Thumbnail for version as of 03:33, 22 July 20201,275 × 1,650, 90 pages (3.2 MB) (talk | contribs)FEDLINK - United States Federal Collection integrationoftwe1094534682 (User talk:Fæ/IA books#Fork8) (batch 1993-2020 #19033)

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