Small gas turbine using a second-generation pulse combustor

Author:

Kentfield J. A. C.1,O'Blenes M. J.1

Affiliation:

1. University of Calgary, Calgary, Alberta, Canada

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Reference12 articles.

1. A Simple Pressure-Gain Combustor for Gas Turbines

2. Performance of Pressure-Gain Combustors Without Moving Parts

3. 5Hayek, A. E. "Analysis of a Pulsed Combustor with an Entrained Secondary Flow," M.Sc. Dissertation,Imperial College, Universityof London, England,1969.

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2. Numerical Investigation of Shrouded Ejector-Enhanced Pulse Combustor Performance at High Pressure;Journal of Propulsion and Power;2017-01

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4. Operability of an Ejector Enhanced Pulse Combustor in a Gas Turbine Environment;46th AIAA Aerospace Sciences Meeting and Exhibit;2008-01-07

5. Ejector Enhanced Pulsejet Based Pressure Gain Combustors: An Old Idea With a New Twist;41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2005-07-10

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