Given the conditions on a converging-diverging wind tunnel. At the reservoir pressure is measured to be 200,000 Pa and density is 1.4 kg/m^3. At the throat section Mach number is 1.0 and speed of sound is 390 m/s. At the exit/exhaust the Mach number is 2.5.

Given the conditions on a converging-diverging wind tunnel. At the reservoir pressure is measured to be 200,000 Pa and density is 1.4 kg/m^3. At the throat section Mach number is 1.0 and speed of sound is 390 m/s. At the exit/exhaust the Mach number is 2.5.

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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Question

8.) What is the Temperature at the exit? *
O 198.54 K
201.79 K
O 203.58 K
O 209.87 K

Given the conditions on a converging-diverging wind tunnel. At the reservoir
pressure is measured to be 200,000 Pa and density is 1.4 kg/m^3. At the throat
section Mach number is 1.0 and speed of sound is 390 m/s. At the exit/exhaust
the Mach number is 2.5.

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