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A Propeller Model Based on a Modern Numerical Lifting-Line Algorithm with an IterativeSemi-Free Wake Solver

A fundamental aerodynamic analysis technique for a single straight fixed wing has been expounded upon and turned into a modern technique that can analyze multiple wings of more realistic shapes common on aircraft. This modern technique is extended further to apply towards propellers. A method to overcome propeller analysis problems at low airspeeds is presented. This method is compared to more traditional propeller analysis techniques.

Identiferoai:union.ndltd.org:UTAHS/oai:digitalcommons.usu.edu:etd-8100
Date01 May 2018
CreatorsMontgomery, Zachary S.
PublisherDigitalCommons@USU
Source SetsUtah State University
Detected LanguageEnglish
Typetext
Formatapplication/pdf
SourceAll Graduate Theses and Dissertations
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