Influence of Compressor Exit Conditions on Combustor Annular Diffusers, Part 1: Diffuser Performance
Author:
Affiliation:
1. Loughborough University, Loughborough,England, LE11 3TU, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.5795
Reference9 articles.
1. Characteristics of combustor diffusers
2. Influence of Compressor Exit Conditions on Diffuser Performance
3. The influence of blade wakes on the performance of combustor shortened prediffusers
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