A steady stream of air at and is brought smoothly to rest at a stagnation point

PHYSICS · Subjective · Fermi University Physics · Fluids & Continuum Physics · Kinematics, conservation laws and ideal flow · Kinematics, conservation laws and ideal flow

Fluid Dynamics, Ch Euler's equation in Lamb's form and the four Bernoulli theorems

Problem

A steady stream of air at

80\,\mathrm{m\,s^{-1}}

and

290\,\mathrm{K}

is brought smoothly to rest at a stagnation point, with

c_p = 1005\,\mathrm{J\,kg^{-1}\,K^{-1}}

for air. Find the temperature rise at the stagnation point.

Browse the problem library