Materials Genome Engineering Advances, EarlyView.During the corrosion of Hf6Ta2O17 by CMAS, stable corrosion products—CaTa2O6 and HfSiO4 form at the interface, which hinder further corrosion of Hf6Ta2O17 by CMAS. This mechanism successfully explains the excellent CMAS corrosion resistance of the Hf6Ta2O17 thermal barrier coating.
Qianqian Zhou +3 more
wiley +1 more source
Investigation of Combustion of the Gas Turbine Engine from Kerosene and Biokerosene and Their Soot Characteristics in Diffusion Flames. [PDF]
ACS Omega, 2022 Hong TD +3 more
europepmc +1 more source
Performance Test of Rateau Turbo-supercharger, the Gas Turbine of which driven by a Roots Blower
, 1935 Ichiro Watanabe, Hirosi Shibata
openalex +2 more sources
Discussion: “Temperature Measurements and Combustion Efficiency in Combustors for Gas-Turbine Engines” (Olson, Walter T., and Bernardo, Everett, 1948, Trans. ASME, 70, pp. 329–333) [PDF]
, 1948 E. F. Frock
openalex +1 more source
A new creep prediction model in Ni‐based superalloys via data‐driven symbolic regression
Materials Genome Engineering Advances, EarlyView.In this study, a predictive model for the creep life of Ni‐based superalloys under service temperature conditions was successfully established by combining high‐throughput data with machine learning algorithms. By employing symbolic regression, an interpretable relationship between the feature parameters and the target performance in the predictive ...
Wenjing Li +6 more
wiley +1 more source
Non-premixed combustion and NOX emission characteristics in a micro gas turbine swirl combustor fueled by methane and ammonia at various heat loads. [PDF]
Heliyon, 2023 Wang Y, Liu J, Wang L, Fu Z, Weng P.
europepmc +1 more source
A high pressure, high temperature combustor and turbine-cooling test facility [PDF]
A new test facility is being constructed for developing turbine-cooling and combustor technology for future generation aircraft gas turbine engines. Prototype engine hardware will be investigated in this new facility at gas stream conditions up to 2480 K
Cochran, R. P., Norris, J. W.
core +1 more source
Towards the development of an efficient low-NOx ammonia combustor for a micro gas turbine
Proceedings of the Combustion Institute, 2019 E. Okafor +6 more
semanticscholar +1 more source
Polymer Composites, EarlyView.Schematic representation of the functionalization, processing steps, and tensile properties of carbon nanotube‐reinforced vinyl ester nanocomposites. Abstract Carbon nanotubes (CNTs) have received significant attention due to their exceptional physical and mechanical properties. Advancements in surface modification techniques have facilitated their use
Yasaman Alaei +4 more
wiley +1 more source
Efficient Power Characteristic Analysis and Multi-Objective Optimization for an Irreversible Simple Closed Gas Turbine Cycle. [PDF]
Entropy (Basel), 2022 Qiu X, Chen L, Ge Y, Shi S.
europepmc +1 more source