Airfoil Stall Suppression by Use of Rectangular Cross Section Burst Control Plates-Reference-Cited by-同舟云学术

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Airfoil Stall Suppression by Use of Rectangular Cross Section Burst Control Plates

Published:2012-01-09 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
language:
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Author:

Nakamura Yushi¹,Rinoie Kenichi¹,Sunada Yasuto¹

Affiliation:

1. University of Tokyo

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-318

Reference20 articles.

1. Low-speed flows involving bubble separations

2. Experimental study of airfoil performance with vortex generators

3. Parametric Study of Vortices Shed from Airfoil Vortex Generators

4. Study of a circulation control airfoil with leading/trailing-edge blowing

5. Delay of airfoil stall by periodic excitation

Cited by 4 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. Airfoil Stall Suppression Effects by Use of Dynamic Bubble Burst Control Plate Utilizing Machine Learning Control;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2020

2. Airfoil Stall Suppression by Use of Bubble Burst Control Plate and Autonomous Actuator System;AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2016

3. Airfoil Stall Suppression Using Feedback-Controlled Rectangular Bubble-Burst Control Plate;Journal of Aircraft;2015-01

4. Airfoil Stall Suppression Using Rectangular Bubble Burst Control Plate and Sensor Actuators;6th AIAA Flow Control Conference;2012-06-25

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