Consider subsonic airflow through a 20-cmdiameter adiabatic duct with inlet conditions of T 1 = 330 K,
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Consider subsonic airflow through a 20-cmdiameter adiabatic duct with inlet conditions of T1 = 330 K, P1 = 180 kPa, and Ma1 = 0.1. Taking the average friction factor to be 0.02, determine the duct length required to accelerate the flow to a Mach number of unity. Also, calculate the duct length at Mach number intervals of 0.1, and plot the duct length against the Mach number for 0.1 ≤ Ma ≤ 1. Discuss the results.
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To determine the duct length required to accelerate the flow to a Mach number of unity and calculate the duct length at Mach number intervals of 01 01 ...View the full answer
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Related Book For 
Fluid Mechanics Fundamentals And Applications
ISBN: 9780073380322
3rd Edition
Authors: Yunus Cengel, John Cimbala
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