Unformatted text preview: 20.55 inches upstream of the nominal onset of uniform flow, the Mach number is 5.8, below the 6.0 exit value. See MACH6M1-EDIT.CL for details and original Sivells code printout. Inviscid Centerline Mach number distribution as predicted using Sivells S.P. Schneider, Purdue AAE 29 Apr 2003 Sivells code output for Mach-6 Nozzle...
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This document was uploaded on 01/12/2012.
- Fall '09