Active Flow Control via Discrete Sweeping and Steady Jets on a Simple-Hinged Flap-Reference-Cited by-同舟云学术

Active Flow Control via Discrete Sweeping and Steady Jets on a Simple-Hinged Flap

Published:2018-08 Issue:8 Volume:56 Page:2961-2973
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Melton LaTunia Pack¹,Koklu Mehti¹,Andino Marlyn¹,Lin John C.¹

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

Funder

Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J056841

Reference28 articles.

1. Delay of airfoil stall by periodic excitation

2. Oscillatory Blowing: A Tool to Delay Boundary-Layer Separation

3. Oscillatory Control of Separation at High Reynolds Numbers

4. Flow Separation Control on a Full-Scale Vertical Tail Model using Sweeping Jet Actuators

5. McLeanJ. D.CrouchJ. D.StonerR. C.SakuraiS.FeifelG. E.FeifelW. M.RushH. M. “Study of the Application of Separation Control by Unsteady Excitation to Civil Transport Aircraft,” NASA CR 1999-209338, 1999.

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