Results 131 to 140 of about 746,875 (274)

Cyclic furnace oxidation of clad WI-52 systems at 1040 C and 1090 C [PDF]

open access: yes
Cyclic furnace oxidation studies were conducted on the cobalt alloy WI-52 clad with Ni-30Cr, Fe-25Cr-4A1, and Ni-20Cr-4A1 foils (0.051 to 0.254 mm thick).
Gedwill, M. A.
core   +1 more source

Creep fatigue life prediction for engine hot section materials (isotropic) [PDF]

open access: yes
A series of high temperature strain controlled fatigue tests have been completed to study the effects of thermomechanical fatigue, multiaxial loading, reactive environments, and imposed mean stresses. The baseline alloy used in these tests was cast B1900+
Levan, G. W.   +2 more
core   +1 more source

Evaluation of coatings for cobalt- and nickel-base superalloys, volume 2 [PDF]

open access: yes
The final results of an oxidation-reduction rig evaluation of aluminide coatings are presented, as applied to 1N-100 and B1900 nickel-base and X-10 and WI-52 cobalt-base alloys.
Brentnall, W. D.   +2 more
core   +1 more source

The Effect of Platinum Layer and Aluminizing Process on Surface Roughness of Coated Superalloy by Pt-Al

open access: yesJournal of Advanced Materials in Engineering, 2019
In this study, the effect of platinum-aluminide coating parameters on surface roughness of nickel-based superalloy Rene®80 was evaluated. For this purpose, different thicknesses of Pt-layer (2, 4, 6 and 8µm) were plated on the Samples.
M. Barjesteh   +3 more
doaj  

Microstructural Characteristics of Al-Ti-B Inoculation Wires and Their Addition to the AlSi7Mg0.3 Alloy. [PDF]

open access: yesMaterials (Basel), 2022
Knaislová A   +6 more
europepmc   +1 more source

Life prediction and constitutive models for engine hot section [PDF]

open access: yes
The purpose of this program is to develop life prediction models for coated anisotropic materials used in gas turbine airfoils. In the program, two single crystal alloys and two coatings are being tested.
Meyer, T. G.   +2 more
core   +1 more source

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