Effects of Distributed Suction on an Airfoil at Low Reynolds Number-Reference-Cited by-同舟云学术

Effects of Distributed Suction on an Airfoil at Low Reynolds Number

Published:2012-03 Issue:3 Volume:50 Page:523-539
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Wahidi Rehda¹,Bridges David H.²

Affiliation:

1. University of Alabama, Tuscaloosa, Alabama 35487

2. Mississippi State University, Mississippi State, Mississippi 39762

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J050913

Reference35 articles.

1. LeBlanc, P. J. "An Experimental Investigation of Transitional Instabilities in Laminar Separation Bubble Flows on Airfoils Operating at Low Reynolds Numbers," Ph.D. Dissertation,Univ. of Southern California, Los Angeles, CA, 1992.

2. Vortex generators used to control laminar separation bubbles

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