STAGNATION FLOW AGAINST CONCAVE SURFACES THAD S. MORTON. Department of Mechanical Engineering Brigham Young University Provo, UT

Size: px

Start display at page:

Download "STAGNATION FLOW AGAINST CONCAVE SURFACES THAD S. MORTON. Department of Mechanical Engineering Brigham Young University Provo, UT"

Winfred Perkins
6 years ago
Views:

1 STAGNATON FLOW AGANST CONCAVE SURFACES THAD S. MORTON Department of Mechanical Engineering Brigham Young Uniersity Proo, UT 8460 Abstract A reiew of preious work relatie to stagnation flow against cured surfaces is presented. The unsteady, three-dimensional nature of stagnation flow against concae surfaces has motiated much research in the context of turbulence. Howeer, an alternatie approach, which could yield aluable insight into the influence of curature on heat transfer at the surface, is that taken by Kirchhoff in analyzing the flat plate with flow separation. An analytical solution for the iniscid elocity profile along a flat plate with separation is presented. The elocity and pressure distributions are compared with those for attached in iscid flow. The application of the method to cured surfaces is discussed. An important issue in aerospace engineering problems is thermal control, inoling a broad range of applications ranging from atmospheric re-entry to the challenge of turbine blade cooling. Currently, the constraint on the turbine inlet temperature imposed by the turbine blade material is the limiting factor in improements in gas turbine efficiency. One of the key mechanisms which influence the estimate of heat transfer to gas turbine blades is the acceleration of the fluid along the surface, due in part to the curature of the surface'. The problem of iniscid stagnation flow past a finite flat plate with separation occurring behind the plate was first studied by Helmholtr. The study was motiated by the inability of the continuous potential flow solution (see Fig. 1) to gie agreement with known alues of pressure coefficient. Kirchhoff 3 then deeloped a general method for handling flows past flat surfaces using the hodograph plane. 4 5 The difficulty with applying the method to cured surfaces will be discussed shortly. The potential flow solution proides an outer boundary condition for the subsequent boundary layer analysis. For instance, in a boundary layer analysis of a flat plate aligned parallel to the free stream, the limiting alue for the elocity far from the plate is simply a constant (equal to the freestream elocity). Goldstein 6 deried the first-order boundary layer equations for flow along a cured surface, and Howarth 7 8 analyzed the neighborhood of a stagnation point on a cured surface assuming a linear ariation in the potential flow elocity with the distance along the wall. Murphy studied unseparated flow along a cured surface along which the free stream potential flow elocity was taken to be constant for the outer boundary condition in the boundary liyer analysis. This, of course, dictated a specific surface shape. He later 10 considered seeral cases; allowing the potential flow elocity to ary by powers of distance along the surface. The cured surface continued to be inestigated 11 1 while a method of matching asymptotic expansions for the outer potential flow and of the inner boundary layer flow began to be de~loped to yield higher-order approximations to the solutions. Van Dyke has pioneered the application of the method as a systematic approach to soling many types of flow problems. Prandtl's original boundary layer assumption is considered to be the first term in an asymptotic expansion describing the boundary layer. The boundary layt=1 expansion, alid only for small alues of some perturbation

parameter (typically inoling Reynolds number), is "matched" with an expansion for the potential flow, alid only for large alues of the perturbation parameter, by summing the two expansions and

2 parameter (typically inoling Reynolds number), is "matched" with an expansion for the potential flow, alid only for large alues of the perturbation parameter, by summing the two expansions and deleting duplicate terms. Howeer, this method does require that the external flow be computed first. 15 The appropriate solution of the iniscid equations to describe limiting flow at large Reynolds number is not known for separated flows, and has a complicated mathematical description for unseparated flow past finite bodies. 16 Also, serious difficulties arise for nonanalytic shapes. With the exception of Kirchhoff's finite flat plate problem, all of the work cited aboe has been restricted to unseparated flows along infinite or semi-infinite surfaces. t is, therefore, aimed primarily at the analysis of laminar, incompressible flows. Schultz-Grunow and Breuer 0 deried the equations for self-similar solutions for a cured surface, leaing the potential flow elocity as an unknown function of flow path, and calculated the special case of constant potential flow elocity. Subsequently, seeral inestigations 1 were made into higher-order solutions to multi-dimensional, incompressible flows free of separation by retaining more terms in the asymptotic expansions. t is known experimentally 5-31 that under some conditions stagnation flow can become unstable, causing stationary Gortler 4 ortices to arise in the boundary layer. Petitjeans 36 noted that Taylor-Gortler instability is a centrifugally drien instability in the boundary layer flow on a concae wall and appears in the form of counter-rotating longitudinal ortices. Theoretical treatments of the phenomenon are also numerous Bogolepo and Lipatoyl 7 analyze asymptotically the uniform flow of a iscous liquid oer a concae surface for large but subcritical Reynolds number. The wakes formed behind a cured plate subjected to an unsteady free stream hae also been inestigated experimentally. 38 Yet there remains to be found a general analytical solution of the potential flow equations for a finite plate with significant curature and at large Reynolds numbers which accounts for flow separation. This information is needed in order to correctly specify the main flow for the boundary layer problem. t is known experimentallf 9 that een at low to moderate Reynolds numbers, separation occurs downstream of a finite plate. The inherent three-dimensional, unsteady nature of the ortices formed at a stagnation point has motiated researchers to consider the concae surface in the context of turbulence. Howeer, for the purposes of estimating the heat transfer at the surface of a cured body, aluable insight might be gained by inestigating the two-dimensional problem by the use of complex ariable theory. Neglecting the ortices would proide a lower bound on the heat transfer estimate. This approach will now be discussed briefly. Until Kirchhoff's treatment of free fluid jets, the conentional method of soling potential flow problems was to find a mapping which transformed some known, closed streamline contour into parallel flow, where the solution was known. This known solution was then mapped back to the closed streamline contour being studied, thereby obtaining the iniscid solution for the actual flow field. But with separation behind the plate, the location of the two streamlines along the discontinuity is unknown. t was Kirchhoff who first recognized that the free surface ~f separation (see Fig. ) could be handled by considering the hodograph plane. n the hodograph plane, the two free streamlines form a cure of constant curature equal to the magnitude of the free stream elocity (Fig. 3 ). Figme 1 Finite plate without separation.! 1:!,

3 p const. Figure Finite plate with separation. 4 Figure 3. Hodograph for flat plate (~-Plane). The objectie of the method is to find a mapping between the hodograph plane and simple parallel flow. For the flat plate case, the hodograph plane can be inerted using the transformation z3 = l/z All elocities and lengths hae been nondimensionalized so that the radius of the arc is unity. The graph of the z 3 -plane, shown in Figure 4, resembles the right half of a doublet. u 3 Figure 4. z3-plane Accordingly, a doublet is then subtracted out of the z 3 plane to gie Z4 = Z3 - a/z3 (where a = 1 ). The result is shown in Fig. 5. Y4 Figure 5. :l.$-plane The Z4-plane can then be rotated by z 5 = 44eiw, and transformed into parallel flow 40 by the transformation ~ = zs Since the complex potential for parallel flow is:

4 the complex potential for the flat plate with separation can be found by back substituting the transformations just listed, to gie: -K =---- (~-w)' 4 [( + 3} _1 ] y=-( -) +tan () t ( + 1) This dimensionless elocity distribution is shown in Figure 6 plotted against that of the flat plate without separation, which approaches infinity due to the infinite curature at the edge. As seen from the figure, both approaches predict a linear eloeity profile in the neighborhood of the stagnation point. The dimensionless pressure is shown in Figure 7. -K Then F = q, + i\jf = 1t ( _1 e-io. - e-;e) e = so that q, = ( 1 ) and \jl = can be rearranged and integrated as follows: K Along the wall, Using the change of ariables + 1 = u gies: " + +1 J J y = -K K,.----; du + 3,---; du u-u-1 uu-l Without Separation With Separation / /" " 0.6 ~y/ 0.4 / \ 0. _/-~ // y Figure 6. Flat Plate Velocity Profile Wtthol.t Separatim..----, //"..!' "/ i / / 0.8 1" -1L ~ y Figure 7. Flat Plate Pressure Distribution ( r.- p~j. ~YzpU 8 The constant, K, can be found to be -- by setting 4+7t y = when = 1, so that 4 The aboe example illustrates one possible procedure for predicting the potential flow past finite concae surfaces with flow separation. The method has traditionally been used only for flow along straight surfaces. The difficulty in applying the method to cured surfaces stems from the fact that the trajectory in the hodograph plane corresponding to the surface is

5 not known as it is in the case of the flat surface. The only piece of information initially aailable for the cured case is that dy dt dy -; = dx = dx = f(x,y) dt where f is known from the surface chosen. So at any point on the surface~ the direction of flow (%) is known, but the magnitude is not. For the flat plate case~ at any point in the hodograph plane corresponding to a point on the surface, the magnitude as well as the direction of flow are known simultaneously. The only unknown is the corresponding location on the actual surface, which is found by soling for the flow field. The straight line in the hodograph plane, together with the semicircle representing flow at the discontinuity downstream, form a closed contour of known shape. The complex potential of some simple flow field, such as parallel flow, is then mapped conformally into the shape of this closed contour just constructed in the hodograph plane. The composition of mappings form a function describing the streamlines in the new configuration. Although the direction and magnitude are both known at the tip of the cured surface, there are infinitely many possible cures connecting the stagnation point to the end point. This is possibility of many different acceleration patterns is shown qualitatiely in Fig. 8. Figure 8. Hodograph of Finite, Cured Plate. u 5 This can also be seen by considering the equations of the surface: x=cose x' =-sin88' and y= sine y' = cos88' The radius, R, of the cure traced by the elocity along the surface in the hodograph plane can be expressed as R=~ =~x'z+y'z R =~(-sine B't + (cose e't R=B' where 8' is some unknown but increasing function of e. Therefore the radius in the hodograph plane increases with increase angle, creating an outward spiral as depicted in Fig. 8. One method of circumenting this problem might be to start first with a known hodograph plane rather than the actual plane. That is, sole the entire flow field for a family of hodograph cures and then determine what surface shape they represent. This reerse approach appears to be quite mathematically inoled, een when simple circular arcs are used in the hodograph. The first choice would be to use a linear fractional transformation to map one of the two points of intersection to the origin and its conjugate to the ideal point. For the third point in the transformation, the origin could be mapped to some point on the real axis, such as x = 1. Howeer, since the actual surface shape will not be known a priori, the simplification obtained in the flat plate case by setting one of the independent ariables to zero is not likely to be possible. This may require numerical integration to obtain the elocity field. Conclusion Numerous researchers hae inestigated stagnation flow on cured surfaces. Due to the difficulty arising from the presence of the wake after separation, many inestigations hae been restricted to unseparated (laminar) flow or to the region immediately neighboring the stagnation point where the elocity profile can be assumed linear. t is thought that two-dimensional complex ariable theory, while unable to predict the three-dimensional ortices which can occur at a stagnation point, could proi~e aluable

6 information as to the influence of concae curature on the heat transfer at the surface. Acknowledgments This research was financed in part by the Rocky Mountain NASA Space Grant Consortium, EL 30, Logan, ljf References 1. Graham, R. W "Fundamental Mechanisms That nfluence The Estimate of Heat Transfer to Gas Turbine Blades," Heat Transfer Engineering, Vol., No., pp Helmholtz, H "On Discontinuous Fluid Motions" (Gennan), Monatsber. Kgl. Akad. Wiss. Berlin, p Kirchhoff: G "The Theory of Free Fluid Jets" (Gennan), Crelles J., Vol Prandtl, L. and Tietjens, 0. G Fundamentals of Hydro- and Aeromechanics, New York, Doer, pp Prandtl, L. and Tietjens, 0. G Applied HydroandAeromechanics, New York, Doer, pp Goldstein, S., Modern Deelopments in Fluid Dynamics, 1st Ed., Vol. 1, pp , Oxford Uniersity Press, Howarth, L "The Boundary Layer in Three Dimensional Flow.-Part. Deriation of the Equations for Flow along a General Cured Surface," Phil. Mag., Vol. 4, p , p Howarth, L "The Boundary Layer in Three Dimensional Flow.-Part. The Flow near a Stagnation Point," Phil. Mag., Vol. 4, p Murphy, J. S "Some Effects of Surface Curature on Laminar Boundary-Layer Flow," J. Aeronaut. Sci., Vol. 0, No.5, pp Murphy, J. S "Similar Solutions for Laminar Boundary-Layer Flow Oer Cured Surfaces," Douglas Aircraft Co. Rep. No. ES Yen, K. T. and Toba, K "A Theory ofthe Two Dimensional Laminar Boundary Layer Oer a Cured Surface," J. Aerospace Sci., Vol. 8, Murphy, J. S "Comment on a Theory of the Two-Dimensional Laminar Boundary Layer Oer a Cured Surface," J. Aerospace Sci., March 196, pp Prandtl, L Hydrodynamic Theory, Vol. 3. p. 90. Berlin: Springer. 14. Lagerstrom, P. A. and Cole, J.D "Examples llustrating Expansion Procedures for the Naier Stokes Equations," J. Rat. Mech. Anal., pp Kaplun, S "The Role ofcoordinate Systems in Boundary Layer Theory," ZAMP, Vol. 5, pp Van Dyke, M "Higher approximations in boundary-layer theory- Part. General analysis," J. FluidMech. Vol. 14, pp Van Dyke, M "Higher approximations in boundary-layer theory- Part. Application to leading edges," J. Fluid Mech. Vol. 14, pp Van Dyke, M Perturbation Methods in Fluid Mechanics, Academic Press, New York. 19. Van Dyke, M "Higher-order boundary layer theory," Annual Reiew of Fluid Mechanics, Vol. 1, edited by W. R. Sears and M. Van Dyke, pp Schultz-Grunow, F. and Breuer, W "Laminar Boundary Layers on Cambered Walls," Basic Deelopments in Fluid Mechanics, M. Holt Editor, Academic Press, New York, NY pp Afzal, N. and Oberai, M. M "Self-similar Solutions of the Second Order Boundary Layer of an ncompressible Fluid with Heat Transfer," nt. J. Heat Mass Transfer, Vol. 15, pp Papenfuss, H. D "Higher-order solutions fur incompressible, three-dimensional boundary-layer flow at the stagnation point of a general body," Archies of Mechanics, Vol. 6, No. 6, pp Singh, B. B. and Singh, J "On the asymptotic behaiors of flows near a stagnation point on a general cured surface." ndian Journal of Theoretical Physics, Vol. 36, No. 1, pp Gortler, H "Uber ein Dreidimensionale lnstabilitat Laminarer Grenzschichten an Konkaen Wanden," Math.-Phys., Kl.:1; also NACA 1M-"" 1375, Tani "Production oflongitudinal Vortices in the Boundary Layer along a Concae Wall," J. Geophysical Res., Vol. 67, No.8, pp So, R. M. and Mellor, G. L "Experiment on Turbulent Boundary Layers on a Concae Wall," Aeronautical Quarterly., Vol. 6, pp Hoffinann, P. H. Muck, K. C., and Bradshaw, P "The effect of concae surface curature on turbulent boundary layers," J. Fluid Mech., Vol. 161, p Barlow, R. S., and Johnston, J.P "Structure of a turbulent boundary layer on a concae surface," J. Fluid Mech. Vol. 191, pp Kim, J., Simon, T. W., and Russ, S.G "Free Stream Turbulence and Concae Curature Effects on Heated, Transitional Boundary Layers," J. Heat Transfer, Trans. ASME, Vol. 114, pp li 1:,, li 6

7 30. Kestoras, M.D. and Simon, T. W "Hydrodynamic and Thermal Measurements in a Turbulent Boundary Layer Recoering From Concae Curature," ASME Journal of Turbomachinery, Vol. 114, pp Kestoras, M.D. and Simon, T. W "Combined Effects of Concae C':lrature and High Free-stream turbulence ntensity of Boundary Layer Heat and Momentum Transport," Presented at the ASME Winter Annual Meeting, New Orleans, No. 8-Dec Daey, A. and Schofield, D "Threedimensional flow near a two dimensional stagnation point," J. Fluid Mech., Vol. 8, pp Kestin, J. and Wood, R. T "On the stability of two-dimensional stagnation flow," J. Fluid Mech., Vol. 44, pp Cheng, E. H. W., Ozisik, M. N., and Williams, J. C "Nonsteady Three-Dimensional Stagnation-Point Flow," Journal of Applied Mechanics, Trans. ASME, March 1971, pp Katagiri, M "Unsteady Boundary Layer Flows at General Three-Dimensional Stagnation Points," Journal of the Physical Society of Japan, Vol. 34, No.1, Petitjeans, P.; Wesfreid, J.E.; Peerhossaini, H "Non-linear inestigation of the Taylor-G6rtler ortices," European Journal of Mechanics, Vol.10, No., p Bogolepo, V.V.; Lipato, "Asymptotic theory of G<Srtler ortices in the boundary layer of a liquid," Journal of Applied Mechanics and Technical Physics, Vol.33, No.3, pp Schobeiri, M. T.; Radke, R. E "Effects of periodic unsteady wake flow and pressure gradient on boundary layer transition along the concae surfitce of a cured plate," ASME Paper 94-GT-37 pp Hudson, J.D. and Dennis, S.C. R "The flow of a iscous incompressible fluid past a normal flat plate at low and intermediate Reynolds numbers: the wake," J. Fluid Mech. Vol. 160, pp Currie,. G Fundamentals Mechanics of Fluids, znd Ed. McGraw Hill, New York, NY, p

SELECTION, SIZING, AND OPERATION OF CONTROL VALVES FOR GASES AND LIQUIDS Class # 6110

SELECTION, SIZING, AND OPERATION OF CONTROL VALVES FOR GASES AND LIQUIDS Class # 6110 SELECTION, SIZIN, AND OERATION OF CONTROL VALVES FOR ASES AND LIUIDS Class # 6110 Ross Turbiille Sales Engineer Fisher Controls International Inc. 301 S. First Aenue Marshalltown, Iowa USA Introduction