Experimental Investigation of the Aerodynamic Lift Response of an Active Finite Gurney Flap-Reference-Cited by-同舟云学术

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Experimental Investigation of the Aerodynamic Lift Response of an Active Finite Gurney Flap

Published:2015-01-03 Issue: Volume: Page:
ISSN:
Container-title:53rd AIAA Aerospace Sciences Meeting
language:
Short-container-title:

Author:

Bach Alena B.¹,Berg Richard¹,Pechlivanoglou Georgios²,Nayeri C.¹,Paschereit Christian O.¹

Affiliation:

1. Technical University of Berlin

2. Smart Blade GmbH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1270

Reference18 articles.

1. Numerical Investigation on the Aerodynamics of Oscillating Airfoils with Deployable Gurney Flaps

2. Gurney flap—Lift enhancement, mechanisms and applications

3. Design of Subsonic Airfoils for High Lift

Cited by 5 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. Dynamic Deployment of a Minitab for Aerodynamic Load Control;Journal of Aircraft;2020-01

2. Unsteady Aerodynamic Model for Deployable Gurney Flaps Based on Indicial Concepts;Journal of Aircraft;2017-07

3. Potential of Retrofit Passive Flow Control for Small Horizontal Axis Wind Turbines;Journal of Engineering for Gas Turbines and Power;2016-10-11

4. Wake Analysis of a Finite Width Gurney Flap;Journal of Engineering for Gas Turbines and Power;2015-11-17

5. Wake Vortex Field of an Airfoil Equipped with an Active Finite Gurney Flap;53rd AIAA Aerospace Sciences Meeting;2015-01-03

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