New Perspectives on the Laminar Boundary Layer Physics in a Polarized Pressure Field with Temperature Gradient: an Analytical Approximation to Blasius Equation

New Perspectives on the Laminar Boundary Layer Physics in a Polarized Pressure Field with Temperature Gradient: an Analytical Approximation to Blasius Equation

Archive of SID Journal of Applied Fluid Mechanics, Vol. 10, No. 4, pp. 1071-1077, 2017. Available online at www.jafmonline.net, ISSN 1735-3572, EISSN 1735-3645. DOI: 10.18869/acadpub.jafm.73.241.27544 New Perspectives on the Laminar Boundary Layer Physics in a Polarized Pressure Field with Temperature Gradient: an Analytical Approximation to Blasius Equation M. Moeini1 and M. R. Chamani2† 1 Department of Civil Engineering, Amirkabir University of Technology, Tehran, Iran 2 Department of Civil Engineering, Isfahan University of Technology, Isfahan, Iran †Corresponding Author Email: [email protected] (Received December 26, 2016; accepted February 8, 2017) ABSTRACT This study proposes a semi-analytic approximation to the laminar boundary layer growth in a polarized pressure field with temperature gradient represented by the joint Blasius-energy equation. We illuminate that f () is a probability density function (PDF) approximated by an amended Gaussian PDF with zero mean and standard deviation 2.18 . This implies a diffusive structure for the molecular momentum conversion as well as the energy flux in the boundary layer. A new limit for the boundary layer edge is also presented. Results suggest an augmented boundary layer when compared to accepted values in the literature. We also reproduce the inverse proportionality of the free stream velocity to the diffusion of both momentum and energy. Keywords: Blasius laminar flow; Semi-analytic approximation; Boundary layer thickness; Momentum diffusion; Energy diffusion. NOMENCLATURE a constant determined to be v crosswise velocity 9.24sqrt (\ nu / U 0) density of fluid c p fluid specific heat f () = uU/ 0 c =erfaU 2 0 0 2 thermal diffusivity Db uniform-pressure momentum constant kinematic viscosity dimensionless temperature defined in Dt uniform-pressure thermal constant Eq. (6) k thermal conductivity * * Stefan–Boltzmann constant k mean absorption coefficient yU0 / x k = 3NR/(3NR+4) 0 **3 Radiation parameter N R kk./4 T , amended Gaussian PDF defined in p piezometric pressure Eq. (9) Pr modified Prandtl number =0 (Mean of the Gaussian Pr Prandtl number distribution) free stream velocity U 0 , Gaussian PDF with mean and T fluid temperature standard deviation temperature of the ambient fluid T =2.18 (Standard deviation of the Gaussian distribution) Tw temperature of the wall u streamwise velocity boundary layer thickness www.SID.ir Archive of SID M. Moeini and M. R. Chamani / JAFM, Vol. 10, No. 4, pp. 1071-1077, 2017. 1. INTRODUCTION analysis (Lari and Moeini, 2015) and the joined differential transform method with the Padè The thorough investigation of inviscid flows led to approximants (Rashidi et al., 2013 and Thiagarajan the increased awareness and development of the and Senthilkumar, 2013). An important outcome boundary layer concept (Schlichting, 1979). This was investigation into more complex physical notion, which was largely evolved by the work of problems. For example, the boundary layer Prandtl, introduced various levels of simplification development was examined under the influence of of the governing equations of fluid flow (Hirsch, magnetic response, with results showing the 2007). A direct consequence was the feasibility of possibility of devaluating the skin friction in an simulation of industrial-scaled applications which orthogonal magnetic field configuration used to be recalcitrant by the full Navier-Stokes (Thiagarajan and Senthilkumar, 2013; and Vyas and equations (Chen et al., 1984; Raptis et al., 2004; Srivastavat, 2012). In addition, several works Rashidi and Erfani, 2011; Lu and Law, 2014). arrived at a simulation for the behavior of non- Newtonian and thixotropic fluids in the boundary One of the most spectacular examples of boundary layers (Sadeqi et al., 2011; Pan et al., 2016 and layers was studied by Blasius almost a century ago. Ashraf et al., 2016) which have been unknown until It was based on the low-speed laminar flow passing quite recently. over a flat plate in a polarized pressure field (Blasius, As a sequel to this corpus, our goal here is to suggest a semi-analytic approximation analogous to 1950). Along with experimental visualizations, results in Ahmad and Al-Barakati (2009), Yun Blasius exploited the Prandtl equations in (2010), Savas (2012) and Bataller (2008) with the conjunction with assumptions about the absence of aim of providing more detailed analysis of the pressure gradient and similarity of velocity profiles laminar boundary layer physics in a polarized to elaborate the so-called Blasius equation. With the pressure field with temperature gradient. The reason help of recursive power series, Blasius (1950) behind the appeal to this approximation, which solved it with satisfying levels of accuracy. makes it preferable to the comparable works, lies in Subsequently, Howarth (1938) performed the its simplicity; In fact, we will justify that through Runge-Kutta method to provide an enhanced this closed-form approximation, the important numerical scheme. properties of boundary layer thickness/diffusion can Due to the engineering significance and be investigated with little computational expense. mathematical value of Blasius equation, there has appeared an extensive body of literature 2. GOVERNING EQUATIONS surrounding it. For instance, Healey (2008) investigated the effect of a controlled point-source The Prandtl equation (Bird et al., 2001, p. 135] disturbance in the Blasius laminar regime. By means of a wave-envelope steepening mechanics, uu1 dpu 2 uv (1) they illustrated the extent to which the flow xy dxy2 becomes nonlinear at low amplitudes. Kuo (2004) presented the solution to the momentum and energy lays the theoretical foundation to identify the equations of Blasius flow in the presence of external flow characteristics. Here, u is the temperature gradient. Zuccher et al. (2006) streamwise velocity, v the crosswise velocity, p the suggested a numerical scheme to solve the whole piezometric pressure and the kinematic viscosity. boundary layer equations with the aim of In the case of a uniform pressure field through the determining the maximum energy growth in a boundary layer, Prandtl equation reduces to the surging instable Blasius flow. Abdallah and Blasius equation (Bird et al. 2001, p. 138] Zeghmati (2011) examined the relative tendency to heat and mass transfer through the boundary layer u f when exposed to buoyancy gradients in the vicinity U of a cylindrical surface. Their results verified the ff 20 f 0 (2) U dominance of mass transfer over energy scattering y 0 when the ratio of Prandtl to Schmidt number x witnessed a significant plummet. Considering the no-slip condition on the plate (u = v On the mathematical side, major advances in = 0 at y = 0) and an asymptotically-reached numerical/analytical techniques have been made to potential flow outside the boundary layer (u = U0 at the need for an enhanced quantification of fluid y = ), Eq. (2) will get subject to motion problems. Such spectrum is very broad ranging from the revelation of homotopy analysis ff001 f (3) 00 (Liao, 1992; Liao, 1999; Bég et al., 2012; Malvandi et al., 2014; Hassan and Rashidi, 2014 and In addition, thermal radiation in the Blasius regime Makukula and Motsa, 2014), differential transforms is typically formulated as (Bataller, 2008) (Rashidi et al., 2013 and Ganji et al., 2016) and Adomian decompositions (Adomian, 1994; Wang, TT 2 T 2004; Aski et al., 2014 and Akpan, 2015) to a uv (4) xyky 2 combination of these and analogous techniques 0 (e.g., coupled integral transform and functional 1072 www.SID.ir Archive of SID M. Moeini and M. R. Chamani / JAFM, Vol. 10, No. 4, pp. 1071-1077, 2017. where T is the temperature, k / c the negative branch of the Gaussian PDF is cut and the p positive values are doubled to keep the thermal diffusivity, k the thermal conductivity, integral ˆ(,)=1(analogous with the integral the fluid specific heat, k0 = 3NR/(3NR+4) where c p **3 N kk.4/ T is the radiation parameter, in Eq. (8) and with the definition of a probability R density function). As a result of a qualitative * k the mean absorption coefficient and * the interpolation, it can be seen that the option 0 Stefan–Boltzmann constant. This PDE can be and 2.18 results in a close consistency between transformed to (Bataller, 2008) the two PDFs (see Fig. (1)). Therefore, Pr k0 ˆ () f () ()=0 (5) f()=(0,) (10) 2 where Pr is the Prandtl number and the dimensionless temprature defined as TT = w (6) TT w where Tw is the temperature of the wall and T the temperature of the ambient fluid. The boundary conditions for Eq. (5) are =0; =1 (7) ||=0 = resulting from the temperature equilibrium at the interface of solid-fluid boundary (T = Tw at y = 0) and the prevailing uniform ambient temperature at the far-field. Fig. 1. Close consistency between the density function f ''\sigma=2.18() and the Amended 3. SEMI-ANALYTICAL Gaussian PDF in Eq. (9). APPROXIMATION The present approximation is based on the This can be validated by solving ODE (10) to obtain hypothesis that a dimensionless quantity taking the closed-form approximation values in the interval [0, 1] can be regarded as a 2 cumulative distribution function (CDF). By 22 2 comparing the CDF against numerical schemes, we fe ()= erf propose a closed-form solution to the ODE in this 2 section, and portray some of its outcomes in section (11) (4). On the grounds of the important property (Iacono and Boyd, 2015) 0 fd fdf f 01 (8) f ″() can be thought of a probability density function (PDF) (Roussas, 2003, p. 34). Vias and Srivastava (2012) and Iacono and Boyd (2015) justified that f″() attains an exponential decline when linearly grows. This provides us with a criterion to the need for a proximate estimation of the PDF. For this purpose, we define an Amended Gaussian function as Fig. 2. Comparison of the suggested approximation f=2.18() with the comparable 20 , schemes in Howarth (1938), Ahmad and Al- , (9) Barakati (2009) and Savas (2012).

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