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Unformatted text preview: he wave segments ef and hi. Consider 4 waves as shown. 2. A two‐dimensional converging diverging nozzle with a design exit Mach number of 2.21 operates with air at a back pressure to chamber pressure ratio of 0.045 producing an underexpanded flow. Sketch the wave pattern that will be produced in the jet (through at least 3 wave reflections) and label the simple and complex wave regions. Compute the Mach number, flow direction and pressure (relative to chamber) at the nozzle exit, and in the first 4 uniform flow regions in th...
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- Spring '14
- Honor Code, Mach number, minimum length nozzle, modified script to [email protected], area Mach number
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