Experiments of Propeller-Induced Flow Effects on a Low-Reynolds-Number Wing-Reference-Cited by-同舟云学术

Experiments of Propeller-Induced Flow Effects on a Low-Reynolds-Number Wing

Published:2018-08 Issue:8 Volume:56 Page:3279-3294
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Ananda Gavin K.¹,Selig Michael S.¹,Deters Robert W.²

Affiliation:

1. University of Illinois at Urbana–Champaign, Urbana, Illinois 61801

2. Embry-Riddle Aeronautical University, Daytona Beach, Florida 32114

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J056667

Reference39 articles.

1. SmeltR.DaviesH. “Estimation of Increase in Lift due to Slipstream,” R&M 1788, Aeronautical Research Council, United Kingdom, 1937.

2. YoungA. D.MorrisD. E. “Note of Flight Tests on the Effect of Slipstream on Boundary Layer Flow,” R&M 1957, Aeronautical Research Council, United Kingdom, 1939.

3. YoungA. D.MorrisD. E. “Further Note of Flight Tests on the Effect of Slipstream on Boundary Layer Flow,” Rept. B.A. 1404b, Royal Aeronautical Establishment, United Kingdom, 1939.

4. ThompsonJ. S.SmeltR.DavisonB.SmithF. “Comparison of Pusher and Tractor Propeller Mounted on a Wing,” R&M 2516, Aeronautical Research Council, United Kingdom, 1940.

5. KuhnR. E.DraperJ. W. “Investigation of the Aerodynamic Characteristics of a Model Wing-Propeller Combination and of the Wing and Propeller Separately at Angles of Attack up to 90 deg,” NACA Rept. 1263, 1956.

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