An Experimental Study of the Near Field Region of a Free Jet with Passive Mixing Tabs

By: Nasa, National Aeronautics and Space Adm

An experimental study was performed to determine the flow characteristics of a tabbed free jet. Results were acquired in the near field (nominally 2 tab widths upstream to 2 tab widths downstream of the exit plane) of a tabbed jet. Upstream pressure results showed static pressure distributions in both the x-and y-directions along the top surface of the tunnel. Hot-wire measurements showed rapid expansion of the core fluid into the ambient region. Two counter rotating regions of streamwise vorticity were shown on each side of the primary tab. An enhancement of the tabbed jet concept was proposed and tested. Specifically, two tabs, half the scale of the primary tab, were added to the primary tab to provide attachment surfaces for the normally occurring ejection of fluid. The secondary tabs caused a slight increase in the streamwise vorticity created from the upstream static pressure gradient while significantly increasing the re-oriented boundary layer vorticity. The combined pumping effect of the two counter rotating regions of vorticity caused a significant increase in the transport of the jet core fluid into the surrounding region. Bohl, D. G. and Foss, J. F. Glenn Research Center DATA ACQUISITION; EXPERIMENTATION; TABS (CONTROL SURFACES); FREE JETS; FLOW CHARACTERISTICS; VORTICITY; UPSTREAM; STATIC PRESSURE; PRESSURE GRADIENTS; PRESSURE DISTRIBUTION; NEAR FIELDS; EJECTION; COUNTER ROTATION; BOUNDARY LAYERS; AUGMENTATION...

• Format: Paperback
• Language: English
• ISBN: 1731565658
• ISBN13: 9781731565655
• Release Date: January 1
• Publisher: Independently Published
• Length: 164 Pages
• Weight: 0.87 lbs.
• Dimensions: 0.3" x 8.5" x 11.0"