Full-Scale Testing of Active Flow Control Applied to a Vertical Tail-Reference-Cited by-同舟云学术

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Full-Scale Testing of Active Flow Control Applied to a Vertical Tail

Published:2019-07 Issue:4 Volume:56 Page:1376-1386
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Lin John C.¹,Whalen Edward A.²,Andino Marlyn Y.¹,Graff Emilio C.³,Lacy Douglas S.⁴,Washburn Anthony E.¹,Gharib Morteza³,Wygnanski Israel J.⁵

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

2. The Boeing Company, Hazelwood, Missouri 63042

3. California Institute of Technology, Pasadena, California 91125

4. The Boeing Company, Seattle, Washington 98124

5. The University of Arizona, Tucson, Arizona 85721

Funder

Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.C034907

Reference21 articles.

1. Fuel Efficiencies Through Airframe Improvements

2. Actuators for Active Flow Control

3. Cavity Resonance Suppression Using Miniature Fluidic Oscillators

4. Parametric Study of Sweeping Jet Actuators for Separation Control

5. Discrete Sweeping Jets as Tools for Improving the Performance of the V-22

Cited by 20 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. Experimental investigation of suction and oscillatory blowing as an alternative for a leading edge slat;Aerospace Science and Technology;2024-08

2. On the need to reassess the design tools for active flow control;Progress in Aerospace Sciences;2024-04

3. Simulation of a confined and a free sweeping air jet impingement cooling from a fluidic oscillator;International Journal of Thermal Sciences;2023-11

4. Compressor and Valve Control Performance Implications on Active Flow Control Aircraft;Journal of Aircraft;2023-11

5. Flow Physics Study of Sweeping Jet Actuation on a NACA 0015 Swept Wing Configuration;AIAA AVIATION 2023 Forum;2023-06-08

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