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que shocks at the exit. (See Figure P6.7.) Determine the number in region R with air as the working fluid.

que shocks at the exit. (See Figure P6.7.) Determine the number in region R with air as the working fluid.

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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What would you have to do to reduce this flow angle to zero degrees?

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6.7 A converging-diverging nozzle is designed to provide flow at Mach 2.0. With the nozzle exhausting to a back pressure of 80 kPa and a reservoir pressure of 280 kPa, the nozzle is overexpanded, with oblique shocks at the exit. (See Figure P6.7.) Determine the flow direction and flow Mach number in region R with air as the working fluid. Reservoir Figure P6.7
Transcribed Image Text:6.7 A converging-diverging nozzle is designed to provide flow at Mach 2.0. With the nozzle exhausting to a back pressure of 80 kPa and a reservoir pressure of 280 kPa, the nozzle is overexpanded, with oblique shocks at the exit. (See Figure P6.7.) Determine the flow direction and flow Mach number in region R with air as the working fluid. Reservoir Figure P6.7
What would you have to do to reduce this flow angle to zero degrees?
Transcribed Image Text:What would you have to do to reduce this flow angle to zero degrees?
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