Fig 8 - uploaded by Zhikai Wang
Content may be subject to copyright.
Ultrasonic dispersion Mg@CuO(CuO:Mg = 1:20).

Ultrasonic dispersion Mg@CuO(CuO:Mg = 1:20).

Source publication
Article
Full-text available
Due to the high cost and long lifecycle of manned Mars exploration missions, in-situ resource utilization technology, including Mg/CO2 processes, has attracted increasing attention. At present, Mg/CO2 engines face the challenges of long ignition delay, serious carbon deposition, and low combustion efficiency. The root of these challenges lies in th...

Similar publications

Article
Full-text available
The blade shape is of great interest to hybrid turbine designers, due to its significant and direct impact on turbine performance. The inlet and outlet diameters of the vane affect the size of the rotor, which is limited because of the small space available in internal combustion engines. The effect of the ratio of the average inlet diameter and th...