Help me solve this problem of dynamic gasesA uniform air stream of Mach number = 3.0 expands through 10°corner as shown in figure. The temperate and pressure of the airstream are 223 K and 25 kPa, respectively. Answer the followings:Unifrom air streamM1, T1, P1Calculate Mach number downstream.the expansion waves2.6 O1.8 O13.9 OCalculate the Fan angle of the.expansion waves2.1 O3.55 O23.56 degrees O42.4 O19.61 degrees OCalculate the pressure downstream9.34 degrees.the expansion wave15.37 degrees O17.45 kPa13.11 degrees O9.8 kPa O7.23 kPa O22.38 degrees O13.38 kPa6.92 kPa O11.22 kPa OCalculate the temperatureThe expansion waves are isentropic*.downstream the expansion wave.(waves (Po1 = Po2154.48 K O35210.56 KFalse130.45 K OTrue170.66 K186.52 K177.36 K Oооo O o C

as per our guidelines i solved 1st 3 questions

Help me solve this problem A uniform air stream of Ma corner as shown in figure. T stream are 223 K and 25 kPa Unifrom air s М, Т, РP Calculate Mach number downstream the expansion waves 2.6 O 1.8 1 3.9 2.1 O 3.55 2.4 O Calculate the pressure downstream .the expansion wave 17.45 kPa O 2 9.8 kPa O 7.23 КРа 13.38 kPa 6.92 kPa O 11.22 kPa O Calculate the temperature downstream the expansion wave 154.48 K O 3 210.56 K O 130.45 K O 170.66 K O

Help me solve this problem A uniform air stream of Ma corner as shown in figure. T stream are 223 K and 25 kPa Unifrom air s М, Т, РP Calculate Mach number downstream the expansion waves 2.6 O 1.8 1 3.9 2.1 O 3.55 2.4 O Calculate the pressure downstream .the expansion wave 17.45 kPa O 2 9.8 kPa O 7.23 КРа 13.38 kPa 6.92 kPa O 11.22 kPa O Calculate the temperature downstream the expansion wave 154.48 K O 3 210.56 K O 130.45 K O 170.66 K O

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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Show work for both subparts as it is a single problem.
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