2007-10-27 05:41:27 · 4 answers · asked by Sridhar Govindaraj NPM 1 in Science & Mathematics ➔ Engineering
First you need to calculate the maximum power requirement (HP) of your centrifugal compressor based upon it's maximum flow rate and it's inlet and discharge pressure requirements.
Then, since you know what the maximum power required is in HP, and I assume you know what your gas turbine drive is rated at in HP, you can calculate the excess power available in the gas turbine driver and express it as a percentage of the total power required for the compressor.
2007-10-27 17:38:31 · answer #1 · answered by gatorbait 7 · 0⤊ 0⤋
The compressor is on the front of the engine. it could the two be a centifugal ( thrust off the area of a wheel) or axial (strait via a tube that's decreased in diameter because of the fact the air is forced via it) form compressor. most of the air is blended with gasoline and ignited, yet maximum folk of the air is used to relax and administration the flame in the engine. different parts of the air are despatched to the cabin to relax and pressurize it. that's extensively utilized to start the different engines on a mutiengine airplane.
2016-12-15 10:37:56 · answer #2 · answered by kostenbauber 4 · 0⤊ 0⤋
P=Mass * Delta Work * Utip speed.
Calculate work from the fuel burnt per lb of mass
2007-10-27 08:39:52 · answer #3 · answered by mavis b 4 · 0⤊ 0⤋
no clue
2007-10-27 05:44:07 · answer #4 · answered by Taylor M 2 · 0⤊ 0⤋