Quantitative and stability study of the evolution of a thermoelastic body. [PDF]
MethodsX, 2023 Zinsou PH, Degla G, Ezzinbi K.
europepmc +1 more source
Some aspects of aircraft jet engine fuels [PDF]
Technologies are reviewed for improving the thermal stability of jet fuels, with reference to the overheating of fuel tanks in supersonic aircraft.
Bekiesinski, R.
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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.
europepmc +1 more source
Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine. 7: Rotor-Blade Fabrication Procedures [PDF]
An experimental investigation was conducted to determine the cooling effectiveness of a wide variety of air-cooled turbine-blade configurations. The blades, which were tested in the turbine of a - commercial turbojet engine that was modified for this ...
Esgar, Jack B., Long, Roger A.
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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
europepmc +1 more source
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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Data regarding dynamic performance predictions of an aeroengine. [PDF]
Data Brief, 2020 De Giorgi MG, Quarta M.
europepmc +1 more source
The design and performance estimates for the propulsion module for the booster of a TSTO vehicle [PDF]
A NASA study of the propulsion systems for possible low-risk replacements for the Space Shuttle is presented. Results of preliminary studies to define the USAF two-stage-to-orbit (TSTO) concept to deliver 10,000 pounds to low polar orbit are described ...
Maldonado, Jaime J. +1 more
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