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uniform supersonic flow of a perfect gas with y = 1.4, a Mach number of 3.0, and an up- eam static pressure of 100 kPa flows over a geometry as shown in Figure P7.8. Deter- ne the downstream static pressure for both profiles. 100 Do

uniform supersonic flow of a perfect gas with y = 1.4, a Mach number of 3.0, and an up- eam static pressure of 100 kPa flows over a geometry as shown in Figure P7.8. Deter- ne the downstream static pressure for both profiles. 100 Do

Elements Of Electromagnetics
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 solve this question step by step and in clear writing. There is a sub question related to the main question. PLEASE ANSWER THAT AS WELL. Thanks!

7.8 A uniform supersonic flow of a perfect gas with y stream static pressure of 100 kPa flows over a geometry as shown in Figure P7.8. Deter- mine the downstream static pressure for both profiles. = 1.4, a Mach number of 3.0, and an up- P1 = 100 kPa р 3 100 kPa M, = 3 M2 M3 M, = 3 M2 M3 a, = 0° az = 0° 10° az = 0° aj = 0° (a) Expansion Fan-Oblique Shock Geometry (b) Oblique Shock-Expansion Fan Geometry Figure P7.8
Transcribed Image Text:7.8 A uniform supersonic flow of a perfect gas with y stream static pressure of 100 kPa flows over a geometry as shown in Figure P7.8. Deter- mine the downstream static pressure for both profiles. = 1.4, a Mach number of 3.0, and an up- P1 = 100 kPa р 3 100 kPa M, = 3 M2 M3 M, = 3 M2 M3 a, = 0° az = 0° 10° az = 0° aj = 0° (a) Expansion Fan-Oblique Shock Geometry (b) Oblique Shock-Expansion Fan Geometry Figure P7.8
Total pressure losses are always bad. Which of these two configurations is better than the other. What should you always do to minimize your total pressure losses?
Transcribed Image Text:Total pressure losses are always bad. Which of these two configurations is better than the other. What should you always do to minimize your total pressure losses?
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