A Preliminary Investigation of the Performance of a Short-length Turbojet Combustor Using Vaporized Hydrocarbon Fuels [PDF]
Two short turbojet combustors designed for use with vaporized hydrocarbon fuels were tested in a one-quarter annular duct. The experimental combustors consisted of many small "swirl-can" combustor elements manifolded together.
Jones, R. E., Pawlik, E. V.
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Quantitative and stability study of the evolution of a thermoelastic body. [PDF]
MethodsX, 2023 Zinsou PH, Degla G, Ezzinbi K.
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, 2022 The oil circuit of a jet engine is required to lubricate and cool mechanical parts. The oil is pumped from the oil tank and flows through heat exchangers. Then it is injected on the bearings for lubrication and cooling, before being scavenged at the bottom of the sumps and finally flows back to the oil tank.
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Effect of thrust and altitude in steep approaches on ground track noise [PDF]
Thrust and altitude effects on ground track noise during steep approaches of four engine, medium range, turbojet ...
Zalovcik, J. A.
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Photographic data on the influence of the composition, preparation method, time and fuel system on the size of water droplets in a fuel-water emulsion. [PDF]
Data Brief, 2022 Niszczota P, Gieras M.
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Investigation of the stall-induced shock wave (hammershock) at the inlet to the engine [PDF]
The peak static pressures measured at the inlet to the engine during stall are presented for a turbojet and two turbofan engines. It is shown for one turbofan and the turbojet that the static pressure ratio across the hammershock does not exceed ...
Kurkov, A. P. +2 more
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Comparison of numerical simulation results of the mixing chamber with physical experiment data
Авіаційно-космічна техніка та технологіяThe mixing chamber of a turbojet engine is the object of the study. The thermogasdynamic processes in the mixing chamber of the turbojet engine before the turbine of the turbofan attachment are the subjects of the study.
Illia Yudin
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Assessment of a regulatory measurement system for the determination of the non-volatile particulate matter emissions from commercial aircraft engines. [PDF]
J Aerosol Sci, 2021 Kinsey JS +27 more
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Summary of recent investigations of inlet flow distortion effect on engine stability [PDF]
A review is presented of recent experimental results, analytical procedures and test techniques employed to evaluate the effects of inlet flow distortion on the stability characteristics of representative afterburning turbofan and turbojet compression ...
Braithwaite, W. M., Graber, E. J., Jr.
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CENTRIFUGAL COMPRESSOR HEAD CHARACTERISTIC OF A MICRO TURBOJET ENGINE BASED ON NUMERICAL SIMULATION
, 2020 Bestoon Najmuldeen Abdullah Abdullah +2 more
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