Performance Enhancement of a Vertical Stabilizer Using Synthetic Jet Actuators: Non-zero Sideslip-Reference-Cited by-同舟云学术

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Performance Enhancement of a Vertical Stabilizer Using Synthetic Jet Actuators: Non-zero Sideslip

Published:2012-06-25 Issue: Volume: Page:
ISSN:
Container-title:6th AIAA Flow Control Conference
language:
Short-container-title:

Author:

Rathay Nicholas¹,Boucher Matthew¹,Amitay Michael¹,Whalen Edward²

Affiliation:

1. Rensselaer Polytechnic Institute

2. The Boeing Company

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2657

Reference27 articles.

1. 1McCormick,B.W.,Aerodynamics,Aeronautics,andFlightMechanics,Wiley,NewYork,NY,1995,pp.513-524.

2. Lift enhancement of an airfoil using a Gurney flap and vortex generators

3. Oscillatory Blowing: A Tool to Delay Boundary-Layer Separation

4. 5Rene, W., Holger, N., Raghu, S., and Wygnanski, I. "Parametric Studyof Sweeping Jet Actuators for Separation Control," AIAAPaper 2010-4247,2010.

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