Register to reply

Compressor section of gas turbine engine duct shaoes

by cw1690
Tags: compressor, duct, engine, shaoes, turbine
Share this thread:
cw1690
#1
Oct30-11, 08:40 AM
P: 10
why convergent rather than divergent? is this to maintain the constant air velocity.
Can someone explain this better to me. Would be helpfull
Phys.Org News Partner Science news on Phys.org
Security CTO to detail Android Fake ID flaw at Black Hat
Huge waves measured for first time in Arctic Ocean
Mysterious molecules in space
duri
#2
Dec25-11, 01:23 PM
P: 3
I wonder why no one replied on this.

This is to take care of density increase in the flow while keeping constant axial velocity. In turbine density decreases do to expansion so passage is divergent.
cw1690
#3
Dec27-11, 06:58 AM
P: 10
Thanks for the late reply to this, I have managed to understand this now. Thanks for your help anyways


Register to reply

Related Discussions
Static pressure in Compressor, Burner, Turbine Aerospace Engineering 0
Turbine and compressor maps Mechanical Engineering 4
Compressor and turbine design Mechanical Engineering 4
How does a jet-engine compressor compress air? Mechanical Engineering 32
Compressor As a Steam Turbine Mechanical Engineering 4