mach6m1-axialmach - 20.55 inches upstream of the nominal...

Info iconThis preview shows page 1. Sign up to view the full content.

View Full Document Right Arrow Icon
axial distance down cl, inches Mach 0 50 100 0 1 2 3 4 5 6 In the inviscid design (nozzle has laminar b.l. displacement correction) Mach 6.0 is reached 75.13 inches downstream of the throat, the nozzle is 101.73 inches long, so uniform flow is reached on the centerline 26.60 inches upstream of the end of the contour. NOTE WELL that the end of the lip of the last nozzle section is 101.975 inches downstream of the throat, because there is a short section of straight contour at the very end of the last nozzle section.
Background image of page 1
This is the end of the preview. Sign up to access the rest of the document.

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...
View Full Document

This document was uploaded on 01/12/2012.

Ask a homework question - tutors are online