Combustion and cooling performance in an aero-engine annular combustor

Essay specific features

 

Issue:

Technology

 

Written by:

James Y

 

Date added:

May 20, 2015

 

Level:

University

 

Grade:

A

 

No of pages / words:

17 / 4622

 

Was viewed:

660 times

 

Rating of current essay:

 
Essay content:

A counter-rotating vortex pair (CRVP) ensures the ignition and flame stability formed in the head zone of the combustor, and the strong injections from the first row of the in-line dilution holes retard flame diffusion downstream. The rotation leads to a non-symmetry of exit temperature distribution...
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The rotation leads to a non-symmetry of exit temperature distribution. The tubes are cooled by the full film from discrete tiny holes with the average diameter 1.5 mm. The flow structures in the downstream zones of several typical cooling holes are analyzed to study the contribution of dilution jets to film formation and cooling performance...
displayed 300 characters

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