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Corrected the question into proper English
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Peter Kämpf
Peter Kämpf
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Why isare there fewer stages in the turbine than in the compressor inof a turbine engine?

Tweeted twitter.com/StackAviation/status/847581125241384960
Post Reopened by mins, Sanchises, Federico, vasin1987, J W
Turned the title into a question, adjusted tags, reworked the body to improve English and legibility. If the number of stages is not the core, feel free to return to your version by using "edited..." button and "rollback" feature.
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mins
mins
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why jet engine Why is there fewer stages in the turbine stage less than in the compressor stagein a turbine engine?

i amI'm a student that interestinterested in aviation so i want. I'd like to askunderstand why jet enginethe turbine stage lesssection has fewer stages than the compressor stagesection in a jet engine. and what affect if we use compressor or

What would be the effects of adding stages to the turbine stage more than, or less than it should be. thanks (sorry for bad english langague skill) ts.to the compressor? How is the optimal number of stages determined?

why jet engine turbine stage less than compressor stage

i am student that interest in aviation so i want to ask why jet engine turbine stage less than compressor stage. and what affect if we use compressor or turbine stage more than or less than it should be. thanks (sorry for bad english langague skill) ts.

Why is there fewer stages in the turbine than in the compressor in a turbine engine?

I'm a student interested in aviation. I'd like to understand why the turbine section has fewer stages than the compressor section in a jet engine.

What would be the effects of adding stages to the turbine, or to the compressor? How is the optimal number of stages determined?

Post Closed as "Needs details or clarity" by DeltaLima♦, Ralph J♦, Pondlife, 60levelchange, reirab
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ts.
ts.
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why jet engine turbine stage less than compressor stage

i am student that interest in aviation so i want to ask why jet engine turbine stage less than compressor stage. and what affect if we use compressor or turbine stage more than or less than it should be. thanks (sorry for bad english langague skill) ts.