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1. Describe the working principle of Pelton turbine.

A 27miles /hr. wind is at 14.65psia pressure at 70°F enters the turbine that has 1000ft? cross sectional area (assume turbine conversion efficiency = 25%). Calculate in Horsepower A.The power of the incoming wind b. Theoretical maximum attainable turbine power

What is different in between Turbines and Compressors.

what is the intake flow in cfm of a 5.3 liter engine running at 6200 RPM with a volumetric efficiency of 86%. If we supercharge it to flow 610 CFM what is the volumetric efficiency?

Please solve Sub parts A,B,C im needed max in 60 minutes thank u, im very needed the solve 1) Air enters the compressor from a Brayton cycle at a pressure of 100 kPa, temperature27oC and a volumetric flow rate of 1A m3/s. If the turbine inlet temperature is 11ACoC and the ratiopressure (B, 1A)*. If the Compressor Efficiency is 8A% and the turbine efficiency is 9B%. Define : A. From the simulation results, show the p-v or T-s diagram of each case study on B. Complete Compressor Power (kW), Turbine Power (kW), Net Work (kW), Heat In(kW), Net Heat (kW), Back work ratio, Thermal Efficiency (% No  Description Pressure ratio=B Ratiopressure=1A 1  Compressor Work (kW)     2  Turbine Work (kW)     3  Net Work (kW)      4  Heat In (kW)     5  Net Heat (kW)     6  Back Work ratio      7  Thermal Efficiency (%)     Attach below is the data from the cyclepad simulation in the form of a cycleproperties (if no answer…

In a diesel engine the fuel is injected at 6.5% of the stroke. The clearance volume is 10% of the stroke. Find the cut off ratio.

What is Gas turbine? Show with the complete diagram.

Derive the velocities relationship between inlet and outlet.

Three disadvantages of parallel compressor systems are _____, _____, and ____.