NASA NTRS · 19880029345
Rectangular subsonic jet flowfield study
Abstract
The flowfield of a rectangular jet with 2:1 aspect ratio was studied at an axial Reynolds number of 127,000, using a three-dimensional laser anemometer. The flowfield surveys resulted in mean velocity vector field plots and contour plots of the Reynolds stress tensor components for the major and minor axes. These data contribute substantially to currently available data of jet flowfields.
Keep this discovery
Explore connections, maps & timelines
Morrison, Gerald L., Tatterson, Gary B., Swan, David H.. 1987-10-01. Rectangular subsonic jet flowfield study. https://ntrs.nasa.gov/citations/19880029345
Cite the original work for its findings. Save a collection to share your selection of sources.