Design and Fabrication Bi-fuel Gas Turbine Combustion Chamber Basis of Turbocharger, M.Sc. Thesis Sharif University of Technology ; Farshchi, Mohammad (Supervisor) ; Hajilouy Benisi, Ali (Co-Advisor)
Abstract
This research is done as a continuation of previous efforts to develop a turbojet engine from a turbocharger at departments of mechanical and aerospace engineering of Sharif University of Technology and describes the necessary steps in order to design and build a dual fuel combustion chamber for a small, turbocharger based turbojet engine. At first, zero-dimensional analysis is done using a code written in Matlab. Using this code, matching of the compressor and turbine in the turbojet thermodynamic cycle is verified and the operating line of the turbojet engine has been extracted. Henceforth, operating conditions of the combustion chamber to start design process is determined. In designing...
Cataloging briefDesign and Fabrication Bi-fuel Gas Turbine Combustion Chamber Basis of Turbocharger, M.Sc. Thesis Sharif University of Technology ; Farshchi, Mohammad (Supervisor) ; Hajilouy Benisi, Ali (Co-Advisor)
Abstract
This research is done as a continuation of previous efforts to develop a turbojet engine from a turbocharger at departments of mechanical and aerospace engineering of Sharif University of Technology and describes the necessary steps in order to design and build a dual fuel combustion chamber for a small, turbocharger based turbojet engine. At first, zero-dimensional analysis is done using a code written in Matlab. Using this code, matching of the compressor and turbine in the turbojet thermodynamic cycle is verified and the operating line of the turbojet engine has been extracted. Henceforth, operating conditions of the combustion chamber to start design process is determined. In designing...
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