The three-dimensional flow organization past a micro-ramp in a supersonic boundary layer-Reference-Cited by-同舟云学术

The three-dimensional flow organization past a micro-ramp in a supersonic boundary layer

Published:2012-05 Issue:5 Volume:24 Page:055105
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Phys. Fluids

Author:

Sun Z.¹,Schrijer F. F. J.¹,Scarano F.¹,van Oudheusden B. W.¹

Affiliation:

1. Aerospace Engineering Department, Delft University of Technology, Kluyverweg 1, 2629HS Delft, The Netherlands

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

Reference29 articles.

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4. Vortex-Generator Model and Its Application to Flow Control

5. K. S. Bohannon, “Passive flow control on civil aircraft flaps using sub-boundary layer vortex generators in the AWIATOR programme,” AIAA Paper No. 2006-2858, 2006.

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