Investigation of the flow through a single-stage two-dimensional nozzle in the Langley 11-inch hypersonic tunnel

Charles H. McLellan, Thomas W. Williams, Ivan E. Beckwith
Dec 1950

Flow surveys have been made in the second of several nozzles to be investigated in the Langley 11-inch hypersonic tunnel. The single-stage, two-dimensional nozzle was designed by the method of characteristics for a Mach number of 7.08 without boundary-layer corrections.

An Adobe Acrobat (PDF) file of the entire report: