Consider subsonic airflow through a 20-cmdiameter adiabatic duct with inlet conditions of T 1 = 330 K, P 1 =

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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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Chapter # 12- COMPRESSIBLE FLOW
Section: Problems
Problem: 111
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Question Posted: September 17, 2023 00:43:24