slip and no-slip boundary conditions over a permeable vertical flat plate on the dimensionless velocity and temperature fields of Blasius laminar boundary layer flow were deeply investigated. By taking similarity variables
the coupled partial differential equations describing the velocity and temperature fields were transformed into nonlinear ordinary differential equations
and then solved numerically using the Runge-Kutta method. The effects of dimensionless parameters on the velocity and temperature fields were investigated with a focus on the analysis of velocity and temperature profiles
with the dimensionless parameters varying under the slip boundary condition. The results indicate that the existence of suction will make the boundary layer thinner
and the boundary layer will be thicker in the case of injection. In contrast with no-slip boundary conditions
the boundary layers of velocity and temperature are all thinner at wall slip boundary conditions. Increasing either the variable viscosity parameter a or the injection and suction parameter will increase the local skin friction coefficient and the local Nusselt number Nu while reducing the velocity and temperature boundary layers thickness. Furthermore
the temperature boundary layer thickness will decrease as the Biot number Bi
Brinkmann number Br decrease or as the Prandtl number Pr and thermal radiation parameter R increase.
Characteristics of entropy generation of Blasius flow over permeable wall vertical flat plate
Aerodynamic performance for bionic drag⁃reducing airfoil
Effect of thermal radiation on the heat transfer performance of a film cooling vane
Numerical simulation of two-phase flow and heat transfer in complex rotating multi-cavity system
Velocity and temperature similarity solutions of wedge flow laminar boundary layer with wall injection
Related Author
MAO Xiao-dong
LIU Yu
SONG Li-ping
ZHAO Guo-chang
Mingming ZHANG
Ziliang ZHANG
宣益民
王天壹
Related Institution
Association of Science and Technology, Shenyang Aerospace University
Liaoning Key Laboratory of Advanced Measurement and Test Technology for Aviation Propulsion System, Faculty of Aerospace Engineering, Shenyang Aerospace University
Institute of Engineering Thermophysics,Chinese Academy of Sciences
Institute of Science and Technology, China Three Gorges Corporation