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Journal Issues
2018 vol. 2
ORIGINAL ARTICLE
Streamlined frameworks for advancing metal based additive manufacturing technologies
J. Glob. Power Propuls. Soc. 2018;2:317-328
ORIGINAL ARTICLE
The sensitivity of 3D separations in multi-stage compressors
J. Glob. Power Propuls. Soc. 2018;2:329-343
ORIGINAL ARTICLE
Accelerated thermal profiling of gas turbine components using luminescent thermal history paints
Silvia Araguás Rodríguez, Tomáš Jelínek, Jan Michálek, Álvaro Yáñez González, Fiona Schulte, Christopher Pilgrim, Jorg Feist, Stephen J. Skinner
J. Glob. Power Propuls. Soc. 2018;2:344-361
ORIGINAL ARTICLE
A novel 4-sensor fast-response aerodynamic probe for non-isotropic turbulence measurement in turbomachinery flows
J. Glob. Power Propuls. Soc. 2018;2:362-375
ORIGINAL ARTICLE
Numerical modeling of CO-emissions for gas turbine combustors operating at part-load conditions
J. Glob. Power Propuls. Soc. 2018;2:376-387
ORIGINAL ARTICLE
Correlation between total pressure losses of highly loaded annular diffusers and integral stage design parameters
J. Glob. Power Propuls. Soc. 2018;2:388-401
ORIGINAL ARTICLE
Sweeping jet impingement heat transfer on a simulated turbine vane leading edge
J. Glob. Power Propuls. Soc. 2018;2:402-414
ORIGINAL ARTICLE
Experimental and numerical investigation of blade resonance in a centrifugal compressor for varying gas properties
J. Glob. Power Propuls. Soc. 2018;2:415-428
ORIGINAL ARTICLE
Influence of blade geometry on secondary flow development in a transonic centrifugal compressor
J. Glob. Power Propuls. Soc. 2018;2:429-441
ORIGINAL ARTICLE
Numerical simulations of an intake-compressor system
J. Glob. Power Propuls. Soc. 2018;2:442-452
ORIGINAL ARTICLE
On the challenge of five-hole-probe measurements at high subsonic Mach numbers in the wake of transonic turbine cascades
J. Glob. Power Propuls. Soc. 2018;2:453-464
ORIGINAL ARTICLE
Deterioration effects of coupled blisk blades
J. Glob. Power Propuls. Soc. 2018;2:465-476
ORIGINAL ARTICLE
Aeroelastic assessment of a highly loaded high pressure compressor exposed to pressure gain combustion disturbances
J. Glob. Power Propuls. Soc. 2018;2:477-492
ORIGINAL ARTICLE
Evaluation of ultra-high bypass ratio engines for an over-wing aircraft configuration
J. Glob. Power Propuls. Soc. 2018;2:493-515
ORIGINAL ARTICLE
Design optimization of a multi-stage axial compressor using throughflow and a database of optimal airfoils
J. Glob. Power Propuls. Soc. 2018;2:516-528
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| eISSN: | 2515-3080 |
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