Experimental Investigation of Vortex Flows Behind a Segmented Blunt Trailing Edge-Reference-Cited by-同舟云学术

Experimental Investigation of Vortex Flows Behind a Segmented Blunt Trailing Edge

Published:2013-11 Issue:11 Volume:51 Page:2529-2539
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Deshpande P. J.¹,Sharma S. D.¹

Affiliation:

1. Department of Aerospace Engineering, Indian Institute of Technology Bombay, Mumbai 400 076, India

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J051838

Reference27 articles.

1. Investigation of the flow behind a two-dimensional model with a blunt trailing edge and fitted with splitter plates

2. The Effect of Base Bleed on the Flow behind a Two-Dimensional Model with a Blunt Trailing Edge

3. Visualization of an incompressible wake with base bleed

4. SharmaS. D. “Experimental Study of Low Speed Base Flows of Castellated Blunt Trailing Edge Aerofoils,” Ph.D. Dissertation, Dept. of Aerospace Engineering, Indian Institute of Technology Bombay, Mumbai, India, 1988.

5. The three-dimensional structure of the wake of a circular cylinder

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