Correction to ‘Free convection effect on the oscillatory flow past an infinite, vertical, porous plate with constant suction. I’ (Soundalgekar, V. M. 1973)

In the paper noted in the title we have found a few mistakes and wish to correct them in this note. First we infer from the non-dimensional temperature θ (= ( T ' - T ' ∞ ) / ( T ' w - T ' ∞ )) and the Grashof number G (= ( T ' w - T ' ∞ ) / ∆ T with ∆ T = U 0 v 2 0 / vg x β ) that T ' ∞ only is kept constant and as G varies so does T ' w . For example, as G , being positive, takes increasing values T ' w increases and hence the fluid subsequently gets heated up as a result of heat-balance. Consequently we expect the fluid temperatures θ 0 (say, for a fixed Y ) to increase with positive G and to decrease with negative G and these results are not in evidence from figures 5-7 of Soundalgekar (1973), which are incorrect. That the results incorporated in and depicted by figures 5-7 cannot be all correct may be understood by a simple mathematical reasoning, namely: if E > 0, θ 0 cannot have a minimum as shown in figure 5 because from equation (20) of the reference, θ H 0 < 0 when θ ' 0 = 0 and if E < 0, θ 0 cannot have a maximum as shown in figure 7. Further it is necessary to know the quantitative nature of the errors committed in the paper. Therefore we have reworked out the problem and evaluated on I. B. M. 1620 the numerical values of the dimensionless mean velocity u 0 , the mean skin friction τ and the mean temperature θ 0 . We have found that the mean velocity diagrams, the values of the mean skin friction and the expression (37) for θ 0 are all correct. But the mean temperature profiles as shown in figures 5-7 are all incorrect! The correct values of the dimensionless mean temperature θ 0 have been presented in this note through figures 1-3. It is quite clear that θ 0 , as expected, increases with positive G significantly in the case of air ( P = 0.71). Physically it means that as the plate temperature T ' w increases (positive G increases) the fluid-temperature increases. This behaviour of θ 0 gets duly reversed when G , being negative, takes increasing values (see figure 3, P = 0.71). In the presence of free convection parameter G the mean temperature θ 0 increases as the frictional heating (positive E ) increases, a result in contrast to that reported by Soundalgekar. Moreover when the Prandtl number P is large, the effect of G (positive or negative) on θ 0 is almost insignificant - a result contrary to the one obtained by Soundalgekar.

An analysis of the two-dimensional flow of an incompressible, viscous fluid past an infinite porous plate is presented under the following conditions: (i) the suction velocity normal to the plate is constant, (ii) the free stream velocity oscillates in time about a constant mean, (iii) the plate temperature is constant, (iv) the difference between the temperature of the plate and the free stream is moderately large causing the free convection currents. Approximate solutions for the coupled nonlinear equations are obtained for velocity and temperature field. Expressions for the mean velocity, the mean temperature and the mean skin-friction are derived in part I. The mean velocity, the mean temperature are shown on graphs and the numerical values of the skin friction are entered in table 1. The effects of G (the Grashof number), P (the Prandtl number) and E (the Eckert number), on the mean motion of air and water are described during the course of discussion. Some of the important observations are as follows. There is a reverse flow of the mean velocity profile of fluids, with small Prandtl number, in the boundary layer close to a plate which is being heated by the free convection currents. The mean skin friction increases with more cooling of the plate and decreases with more heating of the plate. In part II of the paper, the fluctuating flow is described.


Author(s):  
Redha Wahidi ◽  
Walid Chakroun ◽  
Sami Al-Fahad

Turbulent boundary layer flows over a flat plate with multiple transverse square grooves spaced 10 element widths apart were investigated. Mean velocity profiles, turbulence intensity profiles, and the distributions of the skin-friction coefficients (Cf) and the integral parameters are presented for two grooved walls. The two transverse square groove sizes investigated are 5mm and 2.5mm. Laser-Doppler Anemometer (LDA) was used for the mean velocity and turbulence intensity measurements. The skin-friction coefficient was determined from the gradient of the mean velocity profiles in the viscous sublayer. Distribution of Cf in the first grooved-wall case (5mm) shows that Cf overshoots downstream of the groove and then oscillates within the uncertainty range and never shows the expected undershoot in Cf. The same overshoot is seen in the second grooved-wall case (2.5mm), however, Cf continues to oscillate above the uncertainty range and never returns to the smooth-wall value. The mean velocity profiles clearly represent the behavior of Cf where a downward shift is seen in the Cf overshoot region and no upward shift is seen in these profiles. The results show that the smaller grooves exhibit larger effects on Cf, however, the boundary layer responses to these effects in a slower rate than to those of the larger grooves.


The mechanism by means of which momentum is transmitted to a solid surface, in order that it may exert a drag on a fluid flowing past it, is at present understood only very imperfectly. It seems certain, however, that the law of dynamical similarity is applicable to skin friction; if therefore it were possible to measure the tangential force exerted by the wind as it blows over a large tract of land, it should be equal to the skin friction on a similar small surface when subjected to the action of the very high wind which would correspond with the same value of l V/ v . In reducing the tract of land to a similar small flat plate, the trees and houses would be reduced to a mere roughness on the plate. It is to be expected therefore that, if the skin friction on unit area of the earth's surface be expressed in the form F = kp Q 2 s , (1) Q s being the wind velocity near the surface and p the density of air, the constant k will be the same as the constant which would be found in the laboratory by experimenting with a small, slightly roughened plate, if a sufficiently high value of l V/ v , could be obtained. It should be noticed, however, that the velocity which should be compared with is the velocity close to the solid surface and not the general velocity of the air in the case of a flat plate, or the mean velocity over a cross section in the case of flow in a pipe.


Author(s):  
Pranav Joshi ◽  
Joseph Katz

The goal of this research is to study the effect of favorable pressure gradient (FPG) on the near wall structures of a turbulent boundary layer on a smooth wall. 2D-PIV measurements have been performed in a sink flow, initially at a coarse resolution, to characterize the development of the mean flow and (under resolved) Reynolds stresses. Lack of self-similarity of mean velocity profiles shows that the boundary layer does not attain the sink flow equilibrium. In the initial phase of acceleration, the acceleration parameter, K = v/U2dU/dx, increases from zero to 0.575×10−6, skin friction coefficient decreases and mean velocity profiles show a log region, but lack universality. Further downstream, K remains constant, skin friction coefficient increases and the mean velocity profiles show a second log region away from the wall. In the initial part of the FPG region, all the Reynolds stress components decrease over the entire boundary layer. In the latter phase, they continue to decrease in the middle of the boundary layer, and increase significantly close to the wall (below y∼0.15δ), where they collapse when normalized with the local freestream velocity. Turbulence production and wallnormal transport, scaled with outer units, show self-similar profiles close to the wall in the constant K region. Spanwise-streamwise plane data shows evidence of low speed streaks in the log layer, with widths scaling with the boundary layer thickness.


2006 ◽  
Vol 33 (4) ◽  
pp. 259-280 ◽  
Author(s):  
Gopal Singha ◽  
P.N. Deka

Unsteady viscous incompressible free convection flow of an electrically conducting fluid between two heated vertical parallel plates is considered in the presence of a uniform magnetic field applied transversely to the flow. The induce field along the lines of motion varies transversely to the flow and the fluid temperature changing with time. An analytical solution for velocity, induced field and the temperature distributions are obtained for small and large magnetic Reynolds numbers. The skin-friction at the two plates is obtained. Velocity distribution, induced field and skin-friction are plotted against the distance from the plates. It has been observed that with the increase in Rm, the magnetic Reynolds number, at constant M, the Hartmann number, leads to an increase in the skin-friction gradually. But with the increase in M, at constant Rm, the skin-friction decreases.


1997 ◽  
Vol 119 (3) ◽  
pp. 451-459 ◽  
Author(s):  
D. L. Quintana ◽  
M. Amitay ◽  
A. Ortega ◽  
I. J. Wygnanski

The mean and fluctuating characteristics of a plane, unsteady, laminar, wall jet were investigated experimentally for a constant wall-temperature boundary condition. Temperature and streamwise velocity profiles, including the downstream development of the thermal and hydrodynamic boundary layer thicknesses, were obtained through simultaneous hot and cold wire measurements in air. Even at relatively low temperature differences, heating or cooling of a floor surface sufficiently altered the mean velocity profile in the inner, near-wall region to produce significant effects on the jet stability. Selective forcing of the flow at the most amplified frequencies produced profound effects on the temperature and velocity fields and hence the time-averaged heat transfer and shear stress. Large amplitude excitation of the flow (up to 2 percent of the velocity measured at the jet exit plane) at a high frequency resulted in a reduction in the maximum skin friction by as much as 65 percent, with an increase in the maximum wall heat flux as high as 45 percent. The skin friction and wall heat flux were much less susceptible to low-frequency excitation.


1933 ◽  
Vol 1 (1) ◽  
pp. 19-28
Author(s):  
Walter Tollmien

Abstract In this survey the author first describes certain types of turbulent flow, following which he deals successively with the production of turbulent motion; the instability of the laminar motion; fully developed turbulence; momentum interchange and mixing lengths; and relations between the shearing stress at the wall and the mean velocity distributions. Finally he takes up the calculation of skin friction for simple cases of fully developed turbulence, especially for that of the flat plate. Although the methods outlined have often led to practically useful results, it is the author’s belief that they should be considered only as advances toward the real goal of the turbulence theory. The derivation of turbulence phenomena from the hydrodynamical equations will, in his opinion, be possible only by the application of statistical methods.


Measurements of instantaneous velocity, instantaneous temperature, and the corresponding mean and r. m. s. values, obtained in a range of diffusion flames, are presented. The velocity measurements were obtained with a laser anemometer and the temperature measurements with a thermocouple. The flames were formed by burning methane, town gas and hydrogen at the exit from burner tubes of external diameters 15.0, 9.2, 6.3 and 3.2 mm; the corresponding inside diameters were 13.0, 5.1, 5.1 and 2.5 mm. The mean velocity of the gas at exit from the tube ranged from 0.6 to 5.3 m/s. All flames exhibited discrete frequencies in the vicinity of 11 Hz. The instantaneous velocity and temperature signals were close to sinusoidal, except in the vicinity of the reaction zone where double frequencies and spiky signals were observed. The r. m. s. temperature distributions exhibited minima in the region of the maximum values of mean temperature; the r. m. s. velocity distributions were similar in form but the location of the minimum occurred downstream of the corresponding r. m. s. temperature minimum. The minimum in the r. m. s. velocity and temperature distributions were consistant with the observed frequency doubling and stemmed from the need for the frequency to increase to allow an increase in mean temperature in regions where the instantaneous temperature had attained its adiabatic flame value. A flame model is postulated and shown to represent the many observed features of the oscillating flames. It appears that the oscillations stem from aerodynamic instabilities associated with inflexion points in the local, instantaneous velocity distributions.


2021 ◽  
Vol 12 (5) ◽  
pp. 6280-6296

This work studies the steady two-dimensional MHD free convection flow past an inclined porous plate embedded in the porous medium in the presence of heat source, iSoret effect, and chemical reaction. The non-dimensional governing equations are solved by the perturbation technique. The Rosseland approximation is utilized to describe the radiative heat flux in the energy equation. The effect of magnetic parameter, heat source parameter, radiation parameter, Grashofi number, modified Grashofi number, Schmidt number, Prandtl number, porosity parameter, Soreti number, and chemical reaction on velocity, temperature, concentration profiles, skin friction, Nusselt number, and Sherwood number are mainly focussed in discussion with the help of graphs. It is seen that velocity, concentration, and skin friction fall with the increasing value of chemical reaction. Further, temperature, Nusselt number, and Sherwood number increase with the increasing value of chemical reaction.


Author(s):  
Olalekan O. Shobayo ◽  
D. Keith Walters

Abstract Computational fluid dynamics (CFD) results for turbulent flow and heat transfer in a plane channel are presented. This study presents an idealized fully-developed planar channel flow case for which the mean velocity gradient is non-zero only in the wall-normal direction, and the mean temperature gradient is imposed to be uniform and non-zero in the streamwise or spanwise direction. Previous studies have documented direct numerical simulation results for periodic channel flow with mean temperature gradient in both the streamwise and wall-normal directions, but limited investigations exist documenting the effect of imposed spanwise gradient. The objective of this study is to evaluate turbulent heat flux predictions for three different classes of modeling approach: Reynolds-averaged Navier-Stokes (RANS), large-eddy simulation (LES), and hybrid RANS-LES. Results are compared to available DNS data at Prandtl number of 0.71 and Reynolds number of 180 based on friction velocity and channel half-width. Specific models evaluated include the k-ω SST RANS model, monotonically integrated LES (MILES), improved delayed detached eddy simulation (IDDES), and dynamic hybrid RANS-LES (DHRL). The DHRL model includes both the standard formulation that has been previously documented in the literature as well as a modified version developed specifically to improve predictive capability for flows in which the primary mean velocity and mean temperature gradients are not closely aligned. The modification consists of using separate RANS-to-LES blending parameters in the momentum and energy equations. Results are interrogated to evaluate the performance of the three different model types and specifically to evaluate the performance of the new modified DHRL variant compared with the baseline version.


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