Unformatted text preview: the turn is 310K. What is the angle of the turn? 2. Air flows through a two‐dimensional converging‐diverging nozzle with an exit to throat area ratio of 7. The chamber conditions are 500kPa, 850K and the nozzle is running off design with a back pressure equal to half the design value. a. Determine the back pressure b. Determine the exit pressure c. Determine the angle through which the flow is turned as it leaves the nozzle exit. d. Determine the angles of the leading and trailing waves of the...
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- Spring '14
- Mach number, Honor Code, expansion fan