A Turbine's Question
Thread Starter
Joined: Jun 2004
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From: S089
A Turbine's Question
hi guys.
can anyone quote from any sources the various stages of a Jet turbine's gas velocity and pressure?
I.e. are the following correct??
V = velocity, P = pressure
Induction: Low V Low P
Compression: Low V High P
Combustion: High V High P
Extraction: High V Low P (with bypass) ??
appreciated.
nelson
can anyone quote from any sources the various stages of a Jet turbine's gas velocity and pressure?
I.e. are the following correct??
V = velocity, P = pressure
Induction: Low V Low P
Compression: Low V High P
Combustion: High V High P
Extraction: High V Low P (with bypass) ??
appreciated.
nelson
Joined: Mar 2005
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From: UK
PPRuNe Engineering Dept Apprentice
Joined: Mar 2001
Posts: 295
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From: Deep in the boglands of Western Ireland
I must say, I got the Rolls Royce book about a week ago, and it really does the job for turbine engines. (This from a 2nd year Mech Eng cramming for 10 exams, I'm not even studying the material in college yet.)
Joined: Feb 2002
Aviation Qualifications: AME
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From: UK
hekokimushi
Suck, squeeze, bang, fart is the Otto Cycle for Internal combustion engines.
Strictly speaking a gas turbine is Suck, squeeze, burn, blow.
Unless it surges and then it's Suck, squeeze, bangfart,burn, blow/fart/bang. In any order really.
Suck, squeeze, bang, fart is the Otto Cycle for Internal combustion engines.
Strictly speaking a gas turbine is Suck, squeeze, burn, blow.
Unless it surges and then it's Suck, squeeze, bangfart,burn, blow/fart/bang. In any order really.
