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Performance Analysis of J85 Turbojet Engine Matching Thrust with Reduced Inlet Pressure to the CompressorYarlagadda, Santosh 14 June 2010 (has links)
No description available.
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EXPERIMENTAL INVESTIGATION OF COMPOSITE MATERIAL EROSION CHARACTERISTICS UNDER CONDITIONS ENCOUNTERED IN TURBOFAN ENGINESDRENSKY, GEORGE K. 02 July 2007 (has links)
No description available.
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Návrh malého proudového motoru do 1kN tahu / Design of small jet engine to 1kN thrustGongol, Jakub January 2013 (has links)
This work will be focused on issue of a jet engine. The thesis will be divided into search retrieval part and computational part. In the search retrieval part it will focus on different configurations of jet engines as well as areas of their use. The main part of the thesis will however focus on a calculations where a turbine, compressor and an exhaust nozzle will be designed in order to give a thrust of approximately 1kN. Next step will be determination of an engine charcteristic that will give us a preview on how the engine performance will look like in off-design modes.
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