Results 111 to 120 of about 22,707 (244)
An X‐ray scattering setup designed to capture small‐ and wide‐angle X‐ray scattering on a single, large area detector features a partially transmissive beamstop that facilitates non‐invasive recording of X‐ray beam position and intensity during acquisition of X‐ray scattering images.
Hyun Sun Cho +3 more
wiley +1 more source
Study on Heat Transfer Characteristics of Jet Impingement of Turbine Bending Surface
The architecture of aeroengine air-cooling system channels is notably intricate, with impingement heat transfer standing out as a critical process amidst the complexity.
Fei Zeng +4 more
doaj +1 more source
An investigation of temperature distribution in cooled guide vanes [PDF]
A numerical study to determine the temperature distribution in the guide vane blades of a radial inflow turbine is presented. A computer program was developed which permits the temperature distribution to be calculated when the blade is cooled internally
Hamed, A., Kotwal, R., Tabakoff, W.
core +1 more source
A setup for fielding high‐pressure samples contained in diamond anvil cells (DACs) at the LCLS X‐ray free electron laser is described and example powder X‐ray diffraction data are presented. Future prospects for experimental capabilities in DACs enabled by the LCLS, such as short pulse laser interactions and multiple pulse modes, are discussed.A novel ...
Mungo Frost +13 more
wiley +1 more source
A computer program for the transient thermal analysis of an impingement cooled turbine blade [PDF]
A computer program to calculate transient and steady state temperatures, pressures, and coolant flows in a cooled turbine blade or vane with an impingement insert is described.
Gaugler, R. E.
core +1 more source
This study introduces the Gyroid structure, a type of triply periodic minimal surface (TPMS), for enhanced effusion cooling performance. Conjugate heat transfer simulations are used to compare the flow behavior, pressure loss, and overall cooling ...
Kirttayoth Yeranee +5 more
doaj +1 more source
Comparison of cooling effectiveness of turbine vanes with and without film cooling [PDF]
The cooling effectiveness of three film-cooled vanes were compared to the cooling effectiveness of two non-film-cooled vanes. The comparison indicated that, for the vane configurations and test conditions examined, film cooling had an adverse effect near
Gauntner, D. J. +3 more
core +1 more source
Comparison of heat-transfer test data for a chordwise-finned, impingement-cooled turbine vane tested in a four-vane cascade and a research engine [PDF]
The heat-transfer characteristics of a chordwise-finned, impingement-cooled vane were investigated in both a modified J-57 research engine and a four-vane cascade.
Gladden, H. J., Yeh, F. C.
core +1 more source
Study of Lubricant Jet Flow Phenomena in Spur Gears: Out of Mesh Condition [PDF]
Oil jet lubrication on the disengaging side of a gear mesh was analyzed. Results of the analysis were computerized and used to determine the oil jet impingement depth for several gear ratios and oil jet to pitch line velocity ratios.
Akin, L. S., Townsend, D. P.
core +1 more source
Heat flux characteristics of spray wall impingement with ethanol, butanol, iso-octane, gasoline and E10 fuels [PDF]
Aleiferis, PG +4 more
core +1 more source

