NASA NTRS · 20160011535
Study of the Two-Dimensional Flow Through a Converging-Diverging Nozzle
Abstract
A study of a flow through a straight converging-diverging nozzle of simple design has been made preliminary to studies of other supersonic flows. The diverging part of the nozzle was designed by the Prandtl-Busemann method to give a uniform pressure at its exit of 0.298 times the initial total head, that is, to give a Mach number of 1.436. Schlieren photographs of the flow and pressure-distribution measurements along the diverging part of the nozzle were made. A comparison of the theory with these measurements is presented.
Keep this discovery
Explore connections, maps & timelines
Kantrowitz, Arthur, Street, Robert E., Erwin, John R.. 1943-04-01. Study of the Two-Dimensional Flow Through a Converging-Diverging Nozzle. https://ntrs.nasa.gov/citations/20160011535
Cite the original work for its findings. Save a collection to share your selection of sources.