Turbine for ordnance turbojet engine. 2: Cold-air performance with opened stator [PDF]
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throat area on the performance level of a turbojet engine turbine.
Haas, J. E. +2 more
core +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
Application of binary programming to turbojet engine fault detection
, 1987 C A. BOTSARIS +2 more
openalex +1 more source
Large-Eddy Simulation on the Aerodynamic and Thermal Characteristics in a Micropipe of the Hypersonic Engine Precooler. [PDF]
Micromachines (Basel), 2022 Zhang J, Zou Z, Wang Y.
europepmc +1 more source
Preliminary engineering report for design of a subscale ejector/diffuser system for high expansion ratio space engine testing [PDF]
The design of a subscale jet engine driven ejector/diffuser system is examined. Analytical results and preliminary design drawings and plans are included. Previously developed performance prediction techniques are verified. A safety analysis is performed
Doktor, M. F. +2 more
core +1 more source
Effect of Chevron Nozzles on Turbojet Engine Performance and Jet Noise
, 2017 Gakuyo Tamada +2 more
openalex +1 more source
Operating Experience With The Turbine Technologies Sr 30 Turbojet Engine Test System [PDF]
, 2020 Joseph P. Callinan, Gary Hikiss
openalex +1 more source
Experimental study of ceramic coated tip seals for turbojet engines [PDF]
Ceramic gas-path seals were fabricated and successfully operated over 1000 cycles from flight idle to maximum power in a small turboshaft engine. The seals were fabricated by plasma spraying zirconia over a NiCoCrAlX bond boat on the Haynes 25 substrate.
Biesiadny, T. J. +5 more
core +1 more source
Diagnostics of three-shaft turbojet two-circuit engine by using the dynamic parameters
, 1998 Є. М. Карпов, Artem Karpov
openalex +2 more sources
A denoising method for aeroengine gas path electrostatic signal of low signal-to-noise ratio based on IMFs optimized reconstruction and wavelet threshold. [PDF]
Sci RepYan C, Liu Y, Lu F.
europepmc +1 more source