Date of Award:
5-2018
Document Type:
Thesis
Degree Name:
Master of Science (MS)
Department:
Mechanical and Aerospace Engineering
Committee Chair(s)
Douglas Hunsaker
Committee
Douglas Hunsaker
Committee
Geordie Richards
Committee
Stephen Whitmore
Abstract
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.
Checksum
b16ad75fc08f5669f8f79ec6f27e373b
Recommended Citation
Montgomery, Zachary S., "A Propeller Model Based on a Modern Numerical Lifting-Line Algorithm with an Iterative Semi-Free Wake Solver" (2018). All Graduate Theses and Dissertations, Spring 1920 to Summer 2023. 7001.
https://digitalcommons.usu.edu/etd/7001
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