Modification of subsonic wakes using boundary layer and base mass transfer-Reference-Cited by-同舟云学术

Modification of subsonic wakes using boundary layer and base mass transfer

Published:1983-05 Issue:5 Volume:21 Page:665-670
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Porteiro J. L. F.¹,Przirembel C. E. G.²,Page R. H.¹

Affiliation:

1. Texas A&M University, College Station, Texas

2. Clemson University, Clemson, South Carolina

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.8131

Reference15 articles.

1. Theoretical prediction of base pressure for steady base flow

2. Van Wagenen, R. "A Study of Axially-Symmetric Subsonic Base Flow," Ph.D. Thesis,Dept. of Mechanical Engineering, Universityof Washington, Seattle,1968.

3. Viscid-Inviscid Interaction of Incompressible Separated Flows

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