Experimental verification of principal losses in a regulatory particulate matter emissions sampling system for aircraft turbine engines. [PDF]
Aerosol Sci Technol, 2021 Kittelson DB +25 more
europepmc +1 more source
Durability of zirconia thermal-barrier ceramic coatings on air-cooled turbine blades in cyclic jet engine operation [PDF]
Thermal barrier ceramic coatings of stabilized zirconia over a bond coat of Ni Cr Al Y were tested for durability on air cooled turbine rotor blades in a research turbojet engine.
Jacobs, R. E. +3 more
core +1 more source
Adaptive Fuzzy PID Controller applied to micro turbojet engine
, 2021 A. M. Shehata +2 more
openalex +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.
core +1 more source
Parametric diagnostics of the condition of a dual-flow turbojet engine using neural network simulation of the operating process [PDF]
, 2018 Анас Саидович Гишваров +1 more
openalex +1 more source
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]
Materials (Basel), 2022 Kozakiewicz A, Kieszek R.
europepmc +1 more source
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.
core +1 more source
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.
core +1 more source