The Effects of Swirl Recovery Vanes on Single-Rotation Propeller Aerodynamics and Aeroacoustics-Reference-Cited by-同舟云学术

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The Effects of Swirl Recovery Vanes on Single-Rotation Propeller Aerodynamics and Aeroacoustics

Published:2015-06-18 Issue: Volume: Page:
ISSN:
Container-title:21st AIAA/CEAS Aeroacoustics Conference
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Author:

Sinnige Tomas¹,van Kuijk Jesse J.¹,Lynch Kyle P.¹,Ragni Daniele¹,Eitelberg Georg¹,Veldhuis Leo L.¹

Affiliation:

1. Delft University of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2358

Reference26 articles.

1. Assessment and Optimization of the Aerodynamic and Acoustic Characteristics of a Counter Rotating Open Rotor

2. Experimental and Numerical Investigation of a Contra Rotating Open-Rotor Flowfield

3. Aeroacoustic tests of isolated open rotors at high speed

4. Installation Effects on Contra-Rotating Open Rotor Noise

Cited by 2 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. Propulsion Integration;Power-Based Study of Boundary Layer Ingestion for Aircraft Application;2022-09-15

2. Towards Optimum Swirl Recovery Vanes for Propeller Propulsion Systems;35th AIAA Applied Aerodynamics Conference;2017-06-02

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