Active Flow Control of a High-Lift Supercritical Airfoil with Microjet Actuators-Reference-Cited by-同舟云学术

Active Flow Control of a High-Lift Supercritical Airfoil with Microjet Actuators

Published:2020-05 Issue:5 Volume:58 Page:2053-2069
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Aley Kade Stephen¹,Guha Tufan Kumar¹,Kumar Rajan¹

Affiliation:

1. Florida State University, Tallahassee, Florida 32310

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.J058939

Reference18 articles.

1. MorganH. L. Jr. “Experimental Test Results of Energy Efficient Transport (EET) High-Lift Airfoil in Langley Low-Turbulence Pressure Tunnel,” NASA TM-2002-211780, 2002.

2. High-Lift System for a Supercritical Airfoil: Simplified by Active Flow Control

3. Active Flow Control Activities at NASA Langley

4. LittleJ. “High-Lift Airfoil Separation Control with Dielectric Barrier Discharge Plasma Actuators,” Ph.D. Dissertation, Ohio State Univ., Columbus, OH, 2010.

5. Application of an Integrated Flow and Plasma Actuation Model to an Airfoil

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