This work was supported by of the National Natural Science Foundation of China(No.50906041).
The unsteady cloud cavitation shedding in fuel nozzles greatly influences the flow characteristics and spray break-up of fuel,thereby causing erosion damage.With the application of high-pressure common rail systems in...
The authors gratefully acknowledge the support of the National Science and Technology Major Project(J2019-II-0017-0038);the National Natural Science Foundation of China(NSFC 52206061);Science Center for Gas Turbine Project(P2022-A-II-002-001).
The flow field at the inlet of compressors is generally encountered combined total pressure and swirl distortion for either aircraft engine with S-duct or gas turbine with lateral air intake.This inevitably deteriorat...
supported by the National Natural Science Foundation of China (51906008);the Fundamental Research Funds for Central Universities (YWF-21-BJ-J-822);the National Science and Technology Major Project (2017-Ⅲ-0003-0027)
The turbine blades of aircrafts must be properly cooled to prevent engine failure.Thus,to investigate the influence of the tip structure on the film cooling effect,pressure-sensitive paint test technology was used to ...