DESIGN AND DEVELOPMENT OF A 70 N THRUST CLASS TURBOJET ENGINE
P. E. Trazzi
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Experimental Tests and Numerical Analysis of Aerodynamic Properties of the Composite-Made Jet-Propelled Aerial Target. [PDF]
Frant M +3 more
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Performance of an annual combustor designed for a low-cost turbojet engine [PDF]
Performance tests were conducted on a combustor designed for use in a low-cost turbojet engine. Low-cost features included the use of very inexpensive simplex fuel nozzles and combustor liners of perforated sheet material.
Fear, J. S.
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Evaluation of methods for characterizing the fine particulate matter emissions from aircraft and other diffusion flame combustion aerosol sources. [PDF]
Giannelli R +22 more
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A DLSTM-Network-Based Approach for Mechanical Remaining Useful Life Prediction. [PDF]
Liu Y +5 more
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Measurement of exhaust emissions from two J-58 engines at simulated supersonic cruise flight conditions [PDF]
Emissions of total oxides of nitrogen, unburned hydrocarbons, carbon monoxide, and carbon dioxide from two J-58 afterburning turbojet engines at simulated high-altitude flight conditions are reported. Test conditions included flight speeds from Mach 2 to
Holdeman, J. D.
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Characterizing and Predicting nvPM Size Distributions for Aviation Emission Inventories and Environmental Impact. [PDF]
Durdina L +9 more
europepmc +1 more source
Non-Contact Measurement of Blade Vibration in an Axial Compressor. [PDF]
Przysowa R, Russhard P.
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