Air at a temperature of 25°C and standard atmospheric pressure of 101.3 kPa flows through the nozzle into the pipe where the absolute internal pressure is 85 kPa. The nozzle has a throat diameter of d = 30 mm. Gas constant for air is R = 286.9 J/[kg.K] and its specific heat ratio is k = 1.40. (Figure 1) Figure 1 of 1 Part A Determine the mass flow into the pipe. Express your answer using three significant figures. 195| ΑΣΦ | 41 | vec Submit Previous Answers Request Answer X Incorrect; Try Again; 4 attempts remaining Provide Feedback ? kg/s Next >
Air at a temperature of 25°C and standard atmospheric pressure of 101.3 kPa flows through the nozzle into the pipe where the absolute internal pressure is 85 kPa. The nozzle has a throat diameter of d = 30 mm. Gas constant for air is R = 286.9 J/[kg.K] and its specific heat ratio is k = 1.40. (Figure 1) Figure 1 of 1 Part A Determine the mass flow into the pipe. Express your answer using three significant figures. 195| ΑΣΦ | 41 | vec Submit Previous Answers Request Answer X Incorrect; Try Again; 4 attempts remaining Provide Feedback ? kg/s Next >
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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Air at a temperature of 25∘C∘C and standard atmospheric pressure of 101.3 kPakPa flows through the nozzle into the pipe where the absolute internal pressure is 85 kPakPa . The nozzle has a throat diameter of d� = 30 mmmm . Gas constant for air is R� = 286.9 J/[kg⋅K]J/[kg⋅K] and its specific heat ratio is k� = 1.40. (Figure 1)
Determine the mass flow into the pipe.
Express your answer using three significant figures.
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