The convergent-divergent nozzle in Figure 22 expands and accelerates dry air to supersonic speeds at the outlet, where p2 = 8kPa and T2 = 240K. At the throat p1 = 284 kPa, T1 = 665 K and V1 = 517 m / s. Assuming steady and compressible flow of an ideal gas, estimate (a) the mass flow wn kilograms per hour, (b) the velocity V2, and (c) the match number Ma2
The convergent-divergent nozzle in Figure 22 expands and accelerates dry air to supersonic speeds at the outlet, where p2 = 8kPa and T2 = 240K. At the throat p1 = 284 kPa, T1 = 665 K and V1 = 517 m / s. Assuming steady and compressible flow of an ideal gas, estimate (a) the mass flow wn kilograms per hour, (b) the velocity V2, and (c) the match number Ma2
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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The convergent-divergent nozzle in Figure 22 expands and accelerates dry air to supersonic speeds at the outlet, where p2 = 8kPa and T2 = 240K. At the throat p1 = 284 kPa, T1 = 665 K and V1 = 517 m / s. Assuming steady and compressible flow of an ideal gas, estimate (a) the mass flow wn kilograms per hour, (b) the velocity V2, and (c) the match number Ma2
Transcribed Image Text:Aire-
D1 = 1 cm
Dz = 2,5 cm
22
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