Design and Experimental Validation of Swirl Recovery Vanes for Propeller Propulsion Systems

Li, Q.; Öztürk, Kenan; Ragni, D.; Sinnige, T.; Eitelberg, Georg; Veldhuis, LLM; Yangang, Wang

doi:10.2514/6.2017-3571

Design and Experimental Validation of Swirl Recovery Vanes for Propeller Propulsion Systems

Conference paper (2017)

Authors

Q. Li Flight Performance and Propulsion

Kenan Öztürk Student

D. Ragni Wind Energy

T. Sinnige Flight Performance and Propulsion

Georg Eitelberg Flight Performance and Propulsion

LLM Veldhuis Flight Performance and Propulsion

Wang Yangang Northwestern Polytechnical University

Research Group

Flight Performance and Propulsion

DOI: https://doi.org/10.2514/6.2017-3571

To reference this document use:

http://resolver.tudelft.nl/uuid:b3f21d10-cf4c-4dfb-ba23-034071314e38

More Info

expand_more

Published Date

2017

Language

English

Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Research Group

Flight Performance and Propulsion

Files

2017_AIAA_conference_paper.pdf

(pdf | 1.58 Mb)

- Embargo expired in 09-06-2018

Unknown license