Computational study of effect of tabs on a jet in a cross flow-Reference-Cited by-同舟云学术

Computational study of effect of tabs on a jet in a cross flow

Published:2006-08 Issue:7 Volume:35 Page:712-723
ISSN:0045-7930
Container-title:Computers & Fluids
language:en
Short-container-title:Computers & Fluids

Author:

Reddy D.R.,Zaman K.B.M.Q.

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

Reference29 articles.

1. The effect of vortex generators on a jet in a cross-flow;Zaman;Phys Fluids,1997

2. Zaman KBMQ. Reduction of jet penetration in a cross-flow by using tabs. In: 34th Joint propulsion conference. AIAA paper 98-3276. Cleveland, OH, July 13–15, 1998.

3. Steffen Jr CJ, Reddy DR, Zaman KBMQ. Analysis of flowfield from a rectangular nozzle with delta tabs. AIAA 95-2146, 1995.

4. Computation of three-dimensional compressible flow from a rectangular nozzle with delta tabs;Reddy;J Eng Gas Turb Power,1999

5. NPARC Alliance Technical Team. A user’s guide to NPARC. NPARC Alliance Technical Team, Arnold Engineering Development Center, Arnold Airforce Base, TN, 1994.

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