Gas expands in an isentropic process and the gas pressure reduces from 700kPa to 200kPa. The temperature of the gas prior to expansion is given as 227 C. Determine the temperature of the gas after expansion. Gas expands in an isentropic process and the gas pressure reduces from 700kPa to 200kPa. The temperature of the gas prior to expansion is given as 227 0C. Determine
Gas expands in an isentropic process and the gas pressure reduces from 700kPa to 200kPa. The temperature of the gas prior to expansion is given as 227 C. Determine the temperature of the gas after expansion.
Gas expands in an isentropic process and the gas pressure reduces from 700kPa to 200kPa. The temperature of the gas prior to expansion is given as 227 0C. Determine the temperature of the gas after expansion.
2. Define Mach number. The velocity of an aerofoil section with reference to the medium is given as 300 m/s. Assume the static temperature of the fluid medium is 270C and ᵞ = 1.4. Determine the Mach number for the aerofoil section.
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Can you please clarify the density that is used (103) for which fluid is this density for ?