Affiliation:
1. School of Mechanical Engineering, Cranfield Institute of Technology, Cranfield, Bedfordshire, United Kingdom
Abstract
A simple method is presented for the design of annular diffusers that can take into account the effects of compressibility and of canted configurations by use of the area bisector line. No complex boundary layer calculations are required.
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Cited by
5 articles.
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1. Aerodynamic performance analysis and optimization of a turbine duct with low degree of partial admission;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2017-02-19
2. Diffusers;Gas Turbine Combustion;2010-04-26
3. Effect of inlet swirl on the performance of annular diffusers having the same equivalent cone angle;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2006-02-01
4. Flow Field and Performance Characteristics of Combustor Diffusers: A Basic Study;Journal of Engineering for Gas Turbines and Power;1995-10-01
5. Characteristics of combustor diffusers;Progress in Aerospace Sciences;1995-01