P = 80 kPa T = 380 K Maj = 2.8 Normal shock - L = 3 m

Q: Air at 26 psia, 320°F, and Mach number Ma = 0.7 flows through a duct. Calculate the velocity and the…

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Q: Compressed air from the compressor of a gas turbine enters the combustion chamber at T1 = 700 K, P1…

A: Given:To find:The Mach number at the duct exit.The drop in stagnation pressure.

Q: 17-103 Air enters a rectangular duct at T₁ = 300 K, P₁ = 420 kPa, and Ma, = 2. Heat is transferred…

A: The given information in the problem is shown in the following attached image:

Q: Compressed air from the compressor of a gas turbine enters the combustion chamber at T1 = 700 K, P1…

A: Given:To find:The Mach number at the duct exit.The drop in stagnation pressure.

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Q: Helium is heated as it flows subsonically through a 10 cm × 10 cm square duct. The properties of…

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Q: Consider subsonic Rayleigh flow that is accelerated to sonic velocity (Ma = 1) at the duct exit by…

A: The given subsonic Rayleigh flow is accelerated by supplying heat to the fluid flow at the duct…

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Q: Consider a flat plate with a chord length (from leading to trailing edge) of 1 m. The free-strean…

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Q: Air flowing at 8 psia, 480 R, and Ma1 = 2.0 is forced to undergo a compression turn of 15°.…

A: From Prandtl-Meyer function relation,…

Q: Air enters the diffuser with a velocity of 171 m/s. Determine the flow Mach number at the diffuser…

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Q: Determine the stagnation temperature and stagnation pressure of air that is flowing at 36 kPa, 238…

A: Here I have used the simple equation of stagnation temperature and pressure.

Q: 2. A gas stream (k=1.33) at 100 kPa and 723°C is passing at Mach number 0.7. Its temperature is…

A: To start with, we need to convert the given temperature from Celsius to Kelvin. The conversion…

Q: Air enters a 12-m-long, 5-cm-diameter adiabatic duct at V1 = 70 m/s, T1 = 500 K, and P1 = 300 kPa.…

A: Given: V1=70 m/sT1=500 KP1=300 kPaf=0.023 To determine: The Mach number at the duct exit The exit…

Q: Consider supersonic flow of air through a 7-cm-diameter duct with negligible friction. Air enters…

A: Given Data Properties of air  R = 0.287 Kj/Kg-K CP = 1.005 Kj/Kg-K K=1.4 Inlet condition Ma1 = 1.8,…

Q: • R-134a enters a nozzle at 700 kPa and 120 °C and exits at 400 kPa and 30°C. Mass flows steadily…

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Q: Air is cooled as it flows through a 30-cm-diameter duct. The inlet conditions are Ma1 = 1.2, T01 =…

A: Given, Ma1 = 1.2, T01 = 350 K, P01 = 240 kPa  Ma2 = 2.0 diameter of duct (d) = 30 cm

Q: An ideal gas is to flow isentropically from a large tank where the air is maintained at a tempera…

A: Since you have posted a question with multiple sub-parts, we will provide the solution only to the…