Guidelines for Gridding Simple Flows - The Flat Plate in Laminar Flow

2008 ◽  
Author(s):  
Jr Vaughn ◽  
Milton E.
Keyword(s):  
Laminar Flow ◽  
Flat Plate ◽  
Simple Flows

scholarly journals Laminar flow behind a two-dimensional grid

1948 ◽  
Vol 44 (1) ◽  
pp. 58-62 ◽  
Author(s):  
L. I. G. Kovasznay
Keyword(s):  
Laminar Flow ◽  
Flat Plate ◽  
Two Dimensional ◽  
Laminar Wake ◽  
Solid Bodies

The production of a ‘wake’ behind solid bodies has been treated by different authors. S. Goldstein (1) and S. H. Hollingdale (2) have discussed the laminar wake behind a flat plate, while the wake of a two-dimensional grid has been treated for the turbulent case alone using L. Prandtl's ‘Mischungsweg’ theory by E. Anderlik and Gran Olsson (3), (4).

Heat Transfer in the Laminar Boundary Layer Over an Impulsively Started Flat Plate

1975 ◽  
Vol 97 (3) ◽  
pp. 482-484 ◽  
Author(s):  
C. B. Watkins
Keyword(s):  
Heat Transfer ◽  
Boundary Layer ◽  
Laminar Flow ◽  
Flat Plate ◽  
Constant Temperature ◽  
Laminar Boundary Layer ◽  
Temperature Difference ◽  
Thermal Boundary Layer ◽  
Numerical Solutions ◽  
Prandtl Numbers

Numerical solutions are described for the unsteady thermal boundary layer in incompressible laminar flow over a semi-infinite flat plate set impulsively into motion, with the simultaneous imposition of a constant temperature difference between the plate and the fluid. Results are presented for several Prandtl numbers.

Mass transfer in laminar flow

1954 ◽  
Vol 221 (1144) ◽  
pp. 78-99 ◽  
Keyword(s):  
Boundary Layer ◽  
Mass Transfer ◽  
Natural Convection ◽  
Laminar Flow ◽  
Flat Plate ◽  
The Body ◽  
Liquid Fuels ◽  
Fluid Stream ◽  
Mean Values ◽  
Fluid Properties

Starting from the differential equation of mass transfer in laminar flow and the appropriate boundary condition, expressions are derived for the rate of mass transfer from ( a ) a flat plate in a longitudinal fluid stream, ( b ) a vertical flat plate by natural convection, ( c ) the forward stagnation point of a sphere in a fluid stream. Only outward mass transfer is considered; this corresponds to blowing outwards from the plate at a rate inversely proportional to the boundary-layer thickness. The Kármán-Pohlhausen-Kroujiline method is used. Where appropriate the Prandtl or Schmidt number has been taken as 0⋅71. The calculations are valid for all mass-transfer processes for which a single diffusion coefficient can be ascribed to the diffusing property, but are particularly relevant to the combustion of liquid fuels, for which the outward mass-transfer rates are so high that important deviations occur from boundary-layer profiles without mass transfer. Despite the great temperature variations present in boundary layers with combustion, mean values for the fluid properties are assumed. In the case of natural convection, it is assumed that the body forces on the fluid in the boundary layer are everywhere zero; this leads to a less serious over-estimate of the buoyancy than the usual assumptions which are valid only for small temperature differences.

High-speed laminar flow past a fin–body junction

2013 ◽  
Vol 737 ◽  
pp. 19-55 ◽  
Author(s):  
O. R. Tutty ◽  
G. T. Roberts ◽  
P. H. Schuricht
Keyword(s):  
Laminar Flow ◽  
Flat Plate ◽  
High Speed ◽  
Leading Edge ◽  
Limited Range ◽  
Interaction Region ◽  
Liquid Crystal Thermography ◽  
Heating Effects ◽  
Oil Flow ◽  
Free Stream Mach Number

AbstractInterference heating effects generated by a blunt fin-type protuberance on a flat plate exposed to a hypersonic flow have been investigated experimentally and numerically. Experiments and simulations were carried out at a free-stream Mach number of 6.7 under laminar flow conditions. The surface heating on the plate was measured experimentally using liquid-crystal thermography, which provided quantitative data with high spatial resolution. Complementary surface oil flow and schlieren experiments were also carried out to gain a better understanding of the interference flow field. The effects of fin leading-edge diameter on the heating distribution on the flat plate surface were explored. The results of the experiments and simulations agree well and reveal a highly complex interaction region which extends over seven diameters upstream of the fin. Within the interaction region surrounding the fin, heating enhancements up to ten times the undisturbed flat plate value were estimated from the experimental data. However, the liquid crystals have a limited range, and the numerical simulations indicated localized peak heating many times this value both on the plate and the fin itself.

Sign in / Sign up

Export Citation Format

Share Document