Combustion Limits and Efficiency of Turbojet Engines [PDF]
Combustion must be maintained in the turbojet-engine combustor over a wide range of operating conditions resulting from variations in required engine thrust, flight altitude, and flight speed. Furthermore, combustion must be efficient in order to provide
Barnett, H. C., Jonash, E. R.
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Knowledge-Driven Manufacturing Process Innovation: A Case Study on Problem Solving in Micro-Turbine Machining. [PDF]
Zhang D+6 more
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Experimental cold-flow evaluation of a ram air cooled plug nozzle concept for afterburning turbojet engines [PDF]
A concept for plug nozzles cooled by inlet ram air is presented. Experimental data obtained with a small scale model, 21.59-cm (8.5-in.) diameter, in a static altitude facility demonstrated high thrust performance and excellent pumping characteristics ...
Harrington, D. E., Straight, D. M.
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Thermodynamics, Environmental and Sustainability Impacts of a Turbofan Engine Under Different Design Conditions Considering Variable Needs in the Aviation Industry. [PDF]
Aygun H, Sheikhi MR, Caliskan H.
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A comparison of the chemo- and radiotoxicity of thorium and uranium at different enrichment grades. [PDF]
Rump A+4 more
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DESIGN AND DEVELOPMENT OF A 70 N THRUST CLASS TURBOJET ENGINE
P. E. Trazzi
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Multi-modal LSTM network for anomaly prediction in piston engine aircraft. [PDF]
Khattak WR+3 more
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Artificial Neural Network Structure Optimisation in the Pareto Approach on the Example of Stress Prediction in the Disk-Drum Structure of an Axial Compressor. [PDF]
Kozakiewicz A, Kieszek R.
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