Zobrazeno 1 - 10
of 62
pro vyhledávání: '"Huoxing Liu"'
Publikováno v:
Energies, Vol 15, Iss 24, p 9455 (2022)
A wave rotor optimizes the use of energy resources by enhancing thermodynamic cycles, and further optimization of wave rotor geometry is emerging as an attractive research area. Among the geometric features, the stagger angle of channels lacks suffic
Externí odkaz:
https://doaj.org/article/3b139e56c9584134b3805cc21f34d7a5
Autor:
Le Li, Huoxing Liu
Publikováno v:
Energies, Vol 12, Iss 4, p 736 (2019)
With recent advancements in the development of material and manufacturing technology, the leading edge geometry of turbomachine blades has attracted widespread attention. “Sharp„ leading edges always have a better aerodynamic performance, though
Externí odkaz:
https://doaj.org/article/5f36b4fcd48d4d169660da95b261fb8b
Autor:
Chenyuan Liu, Huoxing Liu
Publikováno v:
Energies, Vol 11, Iss 12, p 3275 (2018)
Leakage flow between the rotor and the stator can cause serious performance degradation of wave rotors which utilize nonsteady shock waves to directly transfer energy from burned gases to precompressed air. To solve this problem, primary flow feature
Externí odkaz:
https://doaj.org/article/93ceea9051aa40cdb5dbaf3bdef8ed30
Publikováno v:
Experimental Heat Transfer. :1-22
Publikováno v:
Chinese Journal of Aeronautics. 35:247-259
A wave rotor is suitable for compact and efficient pressure-exchange between gas flows. This work measured the circumferential pressure distribution of the rotor/stator interfaces and utilized a CFD method to simulate the unsteady pressure waves. The
Publikováno v:
International Journal of Applied Mechanics. 15
Shear stress concentrations may promote damage and failure processes. Quantities of studies have focused on the direct shear loading test, while the analytical model has not yet been studied in depth. Aiming to fill the knowledge gap, the theoretical
Publikováno v:
Chinese Journal of Aeronautics, Vol 34, Iss 2, Pp 79-103 (2021)
The Hypersonic Precooled Combined Cycle Engine (HPCCE), which introduces precooler into traditional hypersonic engine, is regarded as the most promising propulsion system for realizing a single-stage-to-orbit vehicle. The unique demands lead to the a
Publikováno v:
Energy Conversion and Management. 277:116578
High bypass ratio turbofan engine is the dominant side of civil aviation engines market at present. This trendency will not change in the coming decades. In a turbofan engine with high thrust, high mass flow and high bypass ratio, the fan blade is th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::dc7d7c76d56cfb2953171869b0eed9c1
https://doi.org/10.1115/1.0002717v
https://doi.org/10.1115/1.0002717v