DLR Portal
Home|Textversion|Imprint|Sitemap|Contact|How to find us |Deutsch
You are here: Home:Departments:Experimental Methods
Advanced Search
News
Strategy & Mission
Research
Departments
C²A²S²E
Experimental Methods
Fluid Systems
High Speed Configurations
Helicopters
Spacecraft
Technical Acoustics
Transport Aircraft
Supersonic and Hypersonic Technology
Projects
Products
Customers & Partners
Staff
Publications
Jobs & Offers
Students & Diploma thesis'
Service & Links
Contact

Back to article

Transitional flow structures behind a Backward-Facing-Step with 6 mm height at U=6.6 m/s visualized by 3D-vorticity iso-contour surfaces (blue) and one horizontal vector plane at 3.5 mm height with instantaneous 3C-velocity vectors colour coded by the wall-normal component (flow from left)
Previous 3/3
Transitional flow structures behind a Backward-Facing-Step with 6 mm height at U=6.6 m/s visualized by 3D-vorticity iso-contour surfaces (blue) and one horizontal vector plane at 3.5 mm height with instantaneous 3C-velocity vectors colour coded by the wall-normal component (flow from left)
Download this image: Hi-Res JPEG (3.74 MB)
Related Topics
Lasers and Masers
Copyright © 2013 German Aerospace Center (DLR). All rights reserved.