Please only answer STEP 2 question. THIS IS MY 3RD TIME POSTING THE SAME QUESTION AND NOT GETTING THE ANSWER I NEED. DONT SOLVE FOR THE MAIN QUESTION, I NEED THE ANSWER TO THE SECOND PART OF THE QUESTION. Why is the design of this Supersonic Diffuser totally wrong? A normal shock occurs at the inlet to a supersonic diffuser, as shown in Figure P4.2. AJA;is equal to 3.0. Find Me, Pe, and the loss in stagnation pressure (Poi - Poe). Repeat for ashock at the exit. Assume y = 1.4.ii1Mz = 2.5212M = 2.5Р*3D 10 kPaPx = 10 kPa

Shock occurs at the inlet of supersonic diffuser, Ma=m1=2.5po1po1=0.490=A1*A2*, P1po2=0.05853…

Answered: A normal shock occurs at the inlet to a…

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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Please only answer STEP 2 question. THIS IS MY 3RD TIME POSTING THE SAME QUESTION AND NOT GETTING THE ANSWER I NEED. DONT SOLVE FOR THE MAIN QUESTION, I NEED THE ANSWER TO THE SECOND PART OF THE QUESTION.

Why is the design of this Supersonic Diffuser totally wrong?

A normal shock occurs at the inlet to a supersonic diffuser, as shown in Figure P4.2. AJA;
is equal to 3.0. Find Me, Pe, and the loss in stagnation pressure (Poi - Poe). Repeat for a
shock at the exit. Assume y = 1.4.
i
i
1
Mz = 2.5
2
1
2
M = 2.5
Р*3D 10 kPa
Px = 10 kPa

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