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A novel scheme design and numerical study of turbine blade ..:

, In: 1st International Conference on Mechanical System Dynamics (ICMSD 2022),

Lv, D. ; Kong, X. ; Liu, Y.... - p. None , 2022

Link: https://doi.org/10.1049/icp.2022.1910

RT 
T1 <cTitle>1st International Conference on Mechanical System Dynamics (ICMSD 2022)</cTitle>: T1 <Title>A novel scheme design and numerical study of turbine blade trailing edge base on multi-disciplines of flow, thermal, and strength</Title>

UL https://suche.suub.uni-bremen.de/peid=ieee-9997270&Exemplar=1&LAN=DE
				
A1 Lv, D.
A1 Kong, X.
A1 Liu, Y.
A1 Zhou, Y.
A1 Wei, W.
A1 Chen, Y.
YR 2022
K1 aerodynamics
K1 aerospace engines
K1 blades
K1 computational fluid dynamics
K1 cooling
K1 design engineering
K1 numerical analysis
K1 turbines
K1 vortices
K1 scheme design
K1 numerical study
K1 turbine blade trailing edge
K1 comprehensive performance
K1 multidisciplinary coupled designing methods
K1 tougher working environment
K1 modern turbine blades
K1 3rd-gen
K1 4th-gen aero engines
K1 flow resistance
K1 structural strength weakness
K1 structure innovation sound
K1 radially tilted trailing edge
K1 cooling area enlarging
K1 edge design models
K1 numerical simulation methods
K1 traditional trailing edge
K1 performance improvements
K1 designed scheme
K1 local cooling efficiency
K1 turbine blade designing
K1 edge slots
SP None
LK http://dx.doi.org/https://doi.org/10.1049/icp.2022.1910
DO https://doi.org/10.1049/icp.2022.1910
SF ELIB - SuUB Bremen

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