Take atmospheric pressure= $98.1 kN/m^2$, R=287 J/kg, and K=1.4.

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Take atmospheric pressure=

$98.1 kN/m^2$ , R=287 J/kg, and K=1.4.

written 7.2 years ago by

shresthapashu • 350

modified 3.0 years ago by

guravadit223 • 20

Air has a velocity of 1000 km/hr at a pressure of $9.81 kN/m^2$ vaccum and a temperature of $47^0$ C. Compute its stagnation properties and the local Mach number. Take atmospheric pressure= $98.1 kN/m^2$ , R=287 J/kg, and K=1.4.

fluid mechanics

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written 3.0 years ago by

guravadit223 • 20

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