Buy custom Combustion and cooling performance in an aero-engine annular combustor
Essay's paper info
Topic: |
Technology
|
Number of pages / Number of words: |
17 / 4622 |
Essay's paper body
Combustion model
2.4. Radiation model
2.5. Governing equations and CFD solver
3. Result and discussion
3.1. Fuel droplet spray and atomization
3.2. Combustion characters in the tube
3.3. Film cooling on annular tubes
3.3.1. Film performance on different strips
3.3.2. Temperature distribution on tubes along axis
4...
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References
1. Introduction
A combustion chamber is the most heavily thermal load part in an aero engine, in which both ignition and combustion keep going on, and normally whose service life is very short. Since very limit data can be obtained from expensive engine tests due to its serious work environment, CFD is often employed to simulate the complex physical processes in a chamber...
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