Aerodynamic and Aeroacoustic Effects of Swirl Recovery Vanes Length-Reference-Cited by-同舟云学术

Aerodynamic and Aeroacoustic Effects of Swirl Recovery Vanes Length

Published:2019-11 Issue:6 Volume:56 Page:2223-2235
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Avallone F.¹,van den Ende L.¹,Li Q.¹,Ragni D.¹,Casalino D.¹,Eitelberg G.¹,Veldhuis L.¹

Affiliation:

1. Delft University of Technology, 2629HS Delft, The Netherlands

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference29 articles.

1. Aerodynamic and Aeroacoustic Performance of a Propeller Propulsion System with Swirl-Recovery Vanes

2. GuynnM.BertonJ.HallerW.HendricksE.TongM. “Performance and Environmental Assessment of an Advanced Aircraft with Open Rotor Propulsion,” NASA TM-2012-217772, 2012, http://www.sti.nasa.gov.

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

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

5. Design and numerical investigation of swirl recovery vanes for the Fokker 29 propeller

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