Numerical simulation of CO 2 condensation process from CH 4 -CO 2 binary gas mixture in supersonic nozzles

Harnessing Visible Light for CO2 Conversion: The Role of Highly Reduced Phosphomolybdate Crystals as Powerful Photocatalysts

Heterogeneous photocatalysts, characterized by well-defined atomic structures and the capacity for rapid, directional electron transfer, are pivotal in the exploration and development of highly efficient systems for visible-light-driven diluted CO2 reduction. Herein, we constructed highly reduced phosphomolybdates crystalline materials 1-3 to help this process, with the formula of [Co2(C8N3H7)4][Co2(C8N3H7)4(H2O)2][Co(H7P4Mo6O31)2]·8H2O (1), [Ni2(C8N3H7)4(H2O)2][Ni2(C8N3H7)4][Ni(H2O)4][Ni(H6P4Mo6O31)2]·3H2O·2C2H5OH (2), and [Zn2(C8N3H7)2][Zn2(C8N3H7)4][Zn2(C8N3H7)2(H2O)2][Zn(H5P4Mo6O31)2] (3) [C8N3H7 = 2-(1H-pyrazol-3-yl)pyridine]. Specifically, catalyst 1 demonstrated a CO production rate of 3276.4 μmol g-1 h-1 in an environment with 20% CO2 concentration, and an impressively elevated rate of 10740.3 μmol g-1 h-1 in a pure CO2 atmosphere. Steady-state photoluminescence spectroscopy revealed that the directional migration of photoelectrons from the Ru complexes to the catalyst was instrumental in enhancing the catalytic activity. This study provides valuable insights into the rational operation of low-concentration CO2 conversion treatment and the design and synthesis of photocatalysts.

Numerical Investigation of the Influence of Air Contaminants on the Interfacial Heat Transfer in Transonic Flow in a Compressor Rotor

Atmospheric air is a commonly used working fluid in turbomachinery. The air typically contains a certain amount of suspended solid particles, as well as water in the form of vapor or droplets. In the current paper, we focus on the numerical modeling of humid air transonic flow in turbomachinery. In this paper we demonstrate a rarely considered, but as presented herein important influence of air humidity, pollution and liquid water content on the performance of the first stage of the gas turbine compressor and turbofan engine fan (NASA rotors 37 and 67). We also discuss the impact of the interfacial heat transfer associated with steam condensation or water evaporation on the distribution of stagnation parameters at the rotor outlet, the rotor performance, and flow conditions, as well as losses. Results demonstrate the impact of the number of pollution particles and water droplets on the compression process in the analyzed rotors, especially on the Mach number distribution in the blade-to-blade channel. In this paper we highlight that the air pollution and liquid water content, together with such physical phenomena as steam condensation or water droplets evaporation, exert a significant influence on work parameters, losses and efficiency, and thus should be considered in high-velocity airflow simulations.