Aerospace Engineering > GATE 2010 > Isentropic Flow
Consider a 1-D adiabatic, inviscid, compressible flow of air (R=287 J/Kg-K cr=718 J/Kg-K)
through a duct of constant cross-sectional area A=1 m2. If the volumetric flow rate is
Q=680 m3/s and stagnation temperature is T0=580.05 K, then the air temperature inside the
duct is
through a duct of constant cross-sectional area A=1 m2. If the volumetric flow rate is
Q=680 m3/s and stagnation temperature is T0=580.05 K, then the air temperature inside the
duct is
Correct : a
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