6. A gas with R = 187 N-m/(kg-K) and γ = 1.3 flows through a variable area duct. At a certain po

Name: 6. A gas with R = 187 N-m/(kg-K) and γ = 1.3 flows through a variable area duct. At a certain point in the flow, the static pressure and temperature are 80 kPa and 15°C, respectively, while the velocity is 100 m/s. The gas is then isentropically expanded until its velocity is 300 m/s. Determine the pressure, temperature, and Mach number that exist the resulting flow.
Uploaded: 2023-11-29T20:49:38-08:00
Duration: 1 min 42 s
Channel: Dominador Tan
Description: 6. A gas with R = 187 N-m/(kg-K) and γ = 1.3 flows through a variable area duct. At a certain point in the flow, the static pressure and temperature are 80 kPa and 15°C, respectively, while the velocity is 100 m/s. The gas is then isentropically expanded until its velocity is 300 m/s. Determine the pressure, temperature, and Mach number that exist the resulting flow.

For this one for our answer so here for this question we have T1 that is 129 Kelvin, P1 that is

Question

6. A gas with R = 187 N-m/(kg-K) and \(\gamma = 1.3\) flows through a variable area duct. At a certain point in the flow, the static pressure and temperature are 80 kPa and 15°C, respectively, while the velocity is 100 m/s. The gas is then isentropically expanded until its velocity is 300 m/s. Determine the pressure, temperature, and Mach number that exist the resulting flow.

          6. A gas with R = 187 N-m/(kg-K) and \(\gamma = 1.3\) flows through a variable area duct. At a certain point in the flow, the static pressure and temperature are 80 kPa and 15°C, respectively, while the velocity is 100 m/s. The gas is then isentropically expanded until its velocity is 300 m/s. Determine the pressure, temperature, and Mach number that exist the resulting flow.

6. A gas with R = 187 N-m/(kg-K) and γ = 1.3 flows through a variable area duct. At a certain point in the flow, the static pressure and temperature are 80 kPa and 15°C, respectively, while the velocity is 100 m/s. The gas is then isentropically expanded until its velocity is 300 m/s. Determine the pressure, temperature, and Mach number that exist the resulting flow.

Added by Michael B.

University Physics with Modern Physics

Hugh D. Young 14th Edition

Thanks for your feedback!

A gas with R=187N-(m)/(kg-K) and gamma =1.3 flows through a variable area duct. At a certain point in the flow, the static pressure and temperature are 80kPa and 15deg C, respectively, while the velocity is 100(m)/(s). The gas is then isentropically expanded until its velocity is 300(m)/(s). Determine the pressure, temperature, and Mach number that exist the resulting flow. 6. A gas with R = 187 N-m/(kg-K) and y= 1.3 flows through a variable area duct. At a certain point in the flow, the static pressure and temperature are 80 kPa and 15-C, respectively while the velocity is 100 m/s. The gas is then isentropically expanded until its velocity is 300 m/s. Determine the pressure, temperature, and Mach number that exist the resulting flow.