Numerical Investigation of Swirl Recovery Design for Propeller Propulsion Systems-Reference-Cited by-同舟云学术

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Numerical Investigation of Swirl Recovery Design for Propeller Propulsion Systems

Published:2018-06-24 Issue: Volume: Page:
ISSN:
Container-title:2018 Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Li Qingxi¹,Liu Xinyuan¹,Eitelberg Georg¹,Veldhuis Leo L.¹

Affiliation:

1. Delft University of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-3648

Reference35 articles.

1. European Commission, "Annual Analyses of the EU Air Transport Market 2016," URL: https://ec.europa.eu/transport/sites/transport/files/2016_eu_air_transport_industry_analyses_report.pdf

2. International Air Transport Association, "Future of the Airline Industry 2035," URL: https://www.iata.org/policy/Documents/iata-future-airline-industry.pdf

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Aerodynamic and Aeroacoustic Effects of Swirl Recovery Vanes Length;Journal of Aircraft;2019-11

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