This preview shows page 1. Sign up to view the full content.
Unformatted text preview: he pressure is 150 kPa. M=5 10o a. Determine the shock angle, Mach number and pressure just after the turn. b. Determine the reflected shock angle and the Mach number and pressure in the region after TWO reflected shocks. c. Sketch the flow through the diffuser, including arrows showing flow direction. Label the pressures and Mach number in each region of the flow up through the region past the second reflected shock (third shock wave). 4. You are designing a rectangular inlet to a Ramjet engine. The engine has a wedge which can move forward and backward within the rectangular cowling (This is similar to an SR‐71, but in 2‐D). It is desired...
View
Full
Document
This document was uploaded on 02/20/2014.
 Spring '14

Click to edit the document details