Comparison Between Zero Mass Flux Flow Control Methods for Low Speed Airfoil Separation Control-Reference-Cited by-同舟云学术

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Comparison Between Zero Mass Flux Flow Control Methods for Low Speed Airfoil Separation Control

Published:2005-06-06 Issue: Volume: Page:
ISSN:
Container-title:35th AIAA Fluid Dynamics Conference and Exhibit
language:
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Author:

Pern Nan Jou¹,Jacob Jamey¹

Affiliation:

1. University of Kentucky

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-4884

Reference18 articles.

1. Low-Reynolds-Number Airfoils

2. Aerodynamic Flow Control over an Unconventional Airfoil Using Synthetic Jet Actuators

3. Dynamic Stall Control by Periodic Excitation, Part 1: NACA 0015 Parametric Study

4. Flow Separation Control with Microflexural Wall Vibrations

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1. Improving Separation Control with Noise-Robust Variants of Dynamic Mode Decomposition;54th AIAA Aerospace Sciences Meeting;2016-01-02

2. Aeroelastic Deformation and Buckling of Inflatable Wings under Dynamic Loads;48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2007-04-23

3. Aeroelastic Behavior of Inflatable Wings: Wind Tunnel and Flight Testing;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08

4. Characterization of Zero Mass Flux Flow Control for Separation Control of an Adaptive Airfoil;3rd AIAA Flow Control Conference;2006-06-05

5. Flight Control of a UAV with Inflatable Wings with Wing Warping;24th AIAA Applied Aerodynamics Conference;2006-06-05

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