DATA COMPARISON AND RESULTS:

DATA COMPARISON

Results:

   The Mini turbojet engine was successfully designed , fabricated and tested. The engine self sustained at  20 l/min fuel  flow and continued to run for 30 seconds.  The Combustion Chamber wall temperature readings show that the mini turbojet’s flame tube is highly efficient in containing the combustion flame thereby keeping the walls of the combustion chamber at acceptable temperatures. The data comparison shows that the engine has run successfully and well within its limits. The engine could achieve higher performance however  the lack of some instruments for vital parameters and safety reasons prevented us from testing the engine further.