Wind tunnel performance results of swirl recovery vanes as tested with an advanced high speed propeller-Reference-Cited by-同舟云学术

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Wind tunnel performance results of swirl recovery vanes as tested with an advanced high speed propeller

Published:1992-07-06 Issue: Volume: Page:
ISSN:
Container-title:28th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

GAZZANIGA JOHN¹,ROSE GAYLE²

Affiliation:

1. Sverdrup Technology Inc., Brook Park, OH

2. NASA, Lewis Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-3770

Reference38 articles.

1. Foss, R.L., and Hopkins, J.A. "Fuel Conservation Potential for theUseof Turboprop Powerplants," SAEPaper 76-0537,May

2. Biermann, D., and Hartman, E.P. "Wind-TunnelTestsof Four-and Six-Blade Singleand Dual-Rotating Tractor Propellers," NACA Report 747, 1942.

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

2. Numerical simulation of interaction between vane wheel and propeller tip vortex;Ships and Offshore Structures;2019-09-17

3. Numerical Investigation of Configurations with Optimum Swirl Recovery for Propeller Propulsion Systems;AIAA Journal;2019-04

4. Design and Experimental Validation of Swirl-Recovery Vanes for Propeller Propulsion Systems;AIAA Journal;2018-12

5. Aerodynamic and Aeroacoustic Performance of a Propeller Propulsion System with Swirl-Recovery Vanes;Journal of Propulsion and Power;2018-11

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