1. The problem statement, all variables and given/known data Cold air enters a heat exchanger at 400 [K] and exits it at 1200 [K]. At the 0.025 [m2] inlet, the pressure is measured to be 1.0 [MPa] and the velocity is measured to be 3 [m/s]. The area of the exit is also 0.025 [m2] and the pressure here is measured to be 300 [kPa]. What is the velocity exiting the heat exchanger? Use conservation of mass principles. 2. Relevant equations 3. The attempt at a solution So the mass flow rate going in equals the mass flow rate going out. m1=m2 I used this formula to calculate the mass flow rate: m1=ρairA1v1 m=(1.225)(0.025)(3)=0.091875 kg/s Since its an ideal gas, I substituted the mass flow rate equation into the ideal gas equation: P2 =(m/(A2v2))RT2 I found R to be 0.287 kJ/(kg*K) v2=[(0.091874 kg/s)(0.287 kJ/(kg*K))(1200K)]/[(300000 N/m2)(0.025 m2)] I got v2= 4.2189 m/s as my velocity which is incorrect since my answer can only be 20,30,27,or 3.3333 m/s. I can't see what I did wrong.