Mechanical Engineering - Compressors, Gas Dynamics and Gas Turbines
Exercise : Compressors, Gas Dynamics and Gas Turbines - Section 1
- Compressors, Gas Dynamics and Gas Turbines - Section 1
- Compressors, Gas Dynamics and Gas Turbines - Section 2
- Compressors, Gas Dynamics and Gas Turbines - Section 3
- Compressors, Gas Dynamics and Gas Turbines - Section 4
41.
An aftercooler is used to
42.
High air-fuel ratio in gas turbines
43.
The ratio of the volume of free air delivery per stroke to the swept volume of the piston, is known as
44.
If p1, is the pressure of air entering the L.P. cylinder and p2 is the pressure of air leaving the L.P. cylinder (or intercooler pressure), then the ratio of cylinder diameters for a single acting, two stage reciprocating air compressor with complete intercooling is given by (where D1 = Dia. of L.P. cylinder, and D2 = Dia. of H.P. cylinder)
45.
The ratio of the indicated power to the shaft power or brake power of the motor or engine required to drive the compressor, is called
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