Answered: 430 K 50° Shock waves

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

Figure shows the exit of a converging–diverging nozzle,
where an oblique shock pattern is formed. In the exit
plane, which has an area of 15 cm², the air pressure is 16 kPa
and the temperature is 250 K. Just outside the exit shock,
which makes an angle of 50° with the exit plane, the temperature
is 430 K. Estimate (a) the mass flow, (b) the throat
area, (c) the turning angle of the exit flow, and, in the tank
supplying the air, (d ) the pressure and (e) the temperature.

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