NASA NTRS · 19920000181
Computed And Measured Flow In A Turnaround Duct
Abstract
Report presents theoretical and experimental study of subsonic flow of air in 180 degree-turnaround duct of rectangular cross section. Purpose of study to conduct partial simulation of conditions similar to those in axisymmetric duct of Space Shuttle main engine. Part of continuing effort to develop capability to simulate complicated turbulent internal flows with large curvatures like those in rocket engines and turbomachinery.
Keep this discovery
Explore connections, maps & timelines
Monson, Daryl J., Seegmiller, H. Lee, Mcconnaughey, Paul K.. 1992-03-01. Computed And Measured Flow In A Turnaround Duct. https://ntrs.nasa.gov/citations/19920000181
Cite the original work for its findings. Save a collection to share your selection of sources.