Study of Gap Physics of Airfoils with Unsteady Flaps-Reference-Cited by-同舟云学术

Study of Gap Physics of Airfoils with Unsteady Flaps

Published:2013-03 Issue:2 Volume:50 Page:643-650
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Liggett Nicholas¹,Smith Marilyn J.¹

Affiliation:

1. Daniel Guggenheim School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032026

Reference21 articles.

1. Compressible Dynamic Stall Performance of a Variable Droop Leading Edge Airfoil with a Gurney Flap

2. WenzingerC.HarrisT. “Wind Tunnel Investigation of an NACA 23012 Airfoil with Various Arrangements of Slotted Flaps,” NACA TR TM-664, 1939.

3. GothertB.RoberC. “Systematic Investigations of the Effects of Planform and Gap Between the Fixed Surface and Control Surface on Simple Flapped Wings,” NACA TR TM-1206, 1949.

4. Unsteady Aerodynamics of an Airfoil/Flap Combination on a Helicopter Rotor Using Computational Fluid Dynamics and Approximate Methods

5. Unsteady Airfoil with Dynamic Leading- and Trailing-Edge Flaps

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4. Two-Dimensional Experimental Investigation on the Effects of a Fowler Flap Gap and Overlap Size on the Wake Flow Field;Journal of Fluids Engineering;2016-11-03