Zobrazeno 1 - 10
of 31
pro vyhledávání: '"Guotai Feng"'
Publikováno v:
Journal of Hematology & Oncology, Vol 17, Iss 1, Pp 1-45 (2024)
Abstract As the most common form of epigenetic regulation by RNA, N6 methyladenosine (m6A) modification is closely involved in physiological processes, such as growth and development, stem cell renewal and differentiation, and DNA damage response. Me
Externí odkaz:
https://doaj.org/article/1ecab64517f24c6189cf2de766499dc0
Publikováno v:
Journal of Drug Delivery Science and Technology. 83:104351
Publikováno v:
In Chinese Journal of Aeronautics June 2009 22(3):243-249
Publikováno v:
In Chinese Journal of Aeronautics June 2009 22(3):230-236
Publikováno v:
In Chinese Journal of Aeronautics February 2008 21(1):1-7
Publikováno v:
Science in China Series E: Technological Sciences. 52:2305-2315
To further make clear vortex structures in diffusion cascades so as to help understand the mechanisms of vortex affecting loss production, the emergence, evolution and development of secondary flow vortexes, including horse shoe vortex, passage vorte
Publikováno v:
Chinese Journal of Aeronautics. 22(2):145-152
Conjugate calculation methodology is used to simulate the C3X gas turbine vanes cooled with leading edge films of “shower-head” type. By comparing calculated results of different turbulence models with the measured data, it is clear that calculat
Publikováno v:
Chinese Journal of Aeronautics. 19:271-277
A comparison of the results of a computational simulation and an experimental measurement indicates a good agreement between them: the bowed blade lowers the energy loss coefficient of engine by 11% in the simulation and by 13% in the measurement. To
Publikováno v:
Chinese Journal of Aeronautics. 17:142-148
A commercial N-S solver has been employed for simulation and investigation of the unsteady flow field inside the tip clearance of a turbine rotor. The main objective of this paper is to introduce a new method of energy loss calculation for the flow f
Publikováno v:
Journal of Thermal Science. 13:8-15
A multi-stage axial compressor has inherently unsteady flow fields because of the following main reasons: (1) relative positions between rotor and stator airfoil; (2) the buildup of converted wakes lead to complex wake/wake and wake/airfoil interacti