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What is jet engine engine pressure ratio?
The pressure ratio in jet engines is the ratio of pressure between the entrance of the compressor and the exit of the compressor.
What is the hot section of a jet engine the compressor or the turbine?
the hottest point of the jet engine is the combustion chamber
What is sucked into the front of a compressor in a jet engine?
The large opening of the compressor sucks in air to be compressed and burnt in the engine.
What is sucked into the front of a compressor of a jet engine?
The large opening of the compressor sucks in air to be compressed and burnt in the engine.
What is suck in front of a compressor in a jet engine?
The large opening of the compressor sucks in air to be compressed and burnt in the engine.
What is the purpose of the turbine in a jet engine?
To drive the compressor section, therefore 'doing work' on the air to increase the efficiency of the combustion process.
What is sucked into the front of the compressor in a jet engine?
Air and everything else nearby.
What are the types of stator?
the types of statore are compressor, gas turbine, turboprop, and jet engine
The condition that rapidly reduces the efficiency of a centrifugal jet engine compressor would be?
Pressure pulsations
What is sucked into the front compressor in a jet engine?
Air. Air and heat are the basis of the jet. The reason for this is that in the combustion chamber compressed air is ignited. The air flow pushes this reaction out the back of the engine and this= thrust.
What is an air turborocket?
An air turborocket is a jet engine in which a gas generator drives the turbine which drives the inlet compressor.
What is the Difference between apu and jet engine?
A typicial Auxiliary Power Unit (APU) is a turboshaftengine. It is similar to a jet engine with how it's compressor and turbine sections are laid out. However jet engines provide power through thrust (exhaust gas pressure) whereas turboshaft engines provide power through a shaft attached to either the compressor or turbine section.
