Homework Statement
The pressure ratio of an air standard gas-turbine cycle is 8/1 and the inlet conditions to the compressor are 200 KPa and 30C. The turbine is limited to a temperature of 1500K and the compressor and turbine adiabatic efficiencies are 60 and 90 respectively. Calculate...
After some talks with several close family friends(all Engineers) I have decided that i would like to pursue a Maters in Mechanical Engineering. I had a tough time starting out in Engineering failing cal 1 my first time i took it. But after all of that i have strung together all B's this past...
Homework Statement
A gas is enclosed in a container fitted with a piston of cross-sectional area 0.1 m2. The pressure of the gas is maintained constant at 8 kPa, while the gas is heated slowly and the piston moves outward a distance of 40 mm. Heat input to the gas during this process is 42...