Pls help ASAP. Pls answer the sub question only. e 3the6.7 A converging-diverging nozzle is designed to provide flow at Mach 2.0. With the nozzleexhausting to a back pressure of 80 kPa and a reservoir pressure of 280 kPa, the nozzle isoverexpanded, with oblique shocks at the exit. (See Figure P6.7.) Determine the flowdirection and flow Mach number in region R with air as the working fluid.abwahnaHelperSPH3ReservoirRRFigure P6.790-71 What would you have to do to reduce this flow angle to zero degrees?

reduce the flow angle to zero degree ***As per comment i had given the answer only sub question****

Answered: What would you have to do to reduce…

Engineering

Mechanical Engineering

What would you have to do to reduce this flow angle to zero degrees?

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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