Hostname: page-component-cd9895bd7-8ctnn Total loading time: 0 Render date: 2024-12-18T21:47:13.012Z Has data issue: false hasContentIssue false

Laterally converging flow. Part 1. Mean flow

Published online by Cambridge University Press:  20 April 2006

H. D. Murphy
Affiliation:
University of California, Los Alamos National Laboratory, NM 87545
F. W. Chambers
Affiliation:
University of New Mexico, Albuquerque, NM 87131 Present address: Lockheed-Georgia Company, Marietta, GA 30063.
D. M. Mceligot
Affiliation:
University of Arizona, Tucson, AZ 85721

Abstract

Laterally converging flow occurs between two parallel surfaces with an exit hole formed in one. The present study examines the flow at a distance from the exit as a means of investigating an accelerating radial internal flow induced by the lateral convergence and satisfying the boundary-layer approximations. The measurements range from laminar to turbulent conditions, including the intermediate stage referred to by some investigators as laminarizing or laminarescent. The acceleration parameter Kv = (ν/V2)dV/dr ranges from 2·6 × 10−8 to 2·2 × 10×4 and the local Reynolds number varies from 210 to 6·8 × 104 for the data reported; the relation between the Reynolds number and the acceleration parameter was varied by adjusting the convergence angle or the plate spacing. For the main experiment the accelerating region is 86 plate spacings in length. Comparison with numerical predictions for laminar and turbulent flow leads to identification of flow regimes in terms of popular acceleration parameters Kv, Kp = (ν/ρ u3*) dp/dr and Kτ = (ν/ρu3*) (∂τ/∂z)w. Results demonstrate that a potentially turbulent entry flow subjected to accleration due to lateral convergence shows features common to laminarization in accelerating turbulent boundary layers in other geometries. Application of the function A+(Kp) for a modified van Driest wall-region model is examined briefly for the intermediate regime.

Type
Research Article
Copyright
© 1983 Cambridge University Press

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Badri Narayanan, M. A. & Ramjee, V. 1969 On the criteria for reverse transition in a two-dimensional boundary layer flow J. Fluid Mech. 35, 225241.Google Scholar
Bankston, C. A. & Mceligot, D. M. 1970 Turbulent and laminar heat transfer to gases with varying properties in the entry region of circular ducts Int. J. Heat Mass Transfer 13, 319344.Google Scholar
Bellhouse, B. J. & Schultz, D. L. 1966 Determination of mean and dynamic skin friction, separation and transition in low-speed flow with a thin-film heated element J. Fluid Mech. 24, 379400.Google Scholar
Blackwelder, R. F. & Kaplan, R. E. 1976 On the wall structure of the turbulent boundary layer J. Fluid Mech. 76, 89112.Google Scholar
Blackwelder, R. F. & Kovasznay, L. S. G. 1972 Large scale motion of a turbulent boundary layer during relaminarization J. Fluid Mech. 53, 6183.Google Scholar
Bradshaw, P. 1969 A note on reverse transition J. Fluid Mech. 35, 387390.Google Scholar
Bradshaw, P. 1975 Review – Complex turbulent flows. Trans A.S.M.E. I: J. Fluids Engng 97, 146154.
Bradshaw, P. 1976 Complex turbulent flows. In Theoretical and Applied Mechanics (ed. W. T. Koiter), p. 103. North-Holland.
Brown, G. L. 1967 Theory and application of heated films for skin friction measurments. In Proc. Heat Transfer and Fluid Mech. Inst., University of California at San Diego. Stanford University Press.
Chambers, F. W., Murphy, H. D. & Mceligot, D. M. 1983 Laterally converging flow. Part 2. Temporal wall shear stress J. Fluid Mech. 127, 403428.Google Scholar
Driest, E. R. Van 1956 On turbulent flow near a wall. J. Aerospace Sci. 23, 10071011 and 1036.
Freymuth, P. 1977 Frequency response and electronic testing for constant temperature hot-wire anemometers. J. Phys. E: Sci. Instrum. 10, 705710.
Harnett, J. P., Koh, J. C. Y. & Mccomas, S. T. 1962 A comparison of predicted and measured friction factors for turbulent flows through rectangular ducts. Trans. A.S.M.E. C: J. Heat Transfer 84, 8288.
Huffman, G. D. & Bradshaw, P. 1972 A note on von Kármán's constant in low Reynolds number turbulent flows J. Fluid Mech. 53, 4560.Google Scholar
Jones, W. P. & Launder, B. E. 1972 Some properties of sink-flow turbulent boundary layers J. Fluid Mech. 56, 337351.Google Scholar
Kays, W. M. & Crawford, M. E. 1980 Convective Heat and Mass Transfer, 2nd edn. McGraw-Hill.
Kline, S. J. 1967 Observed structure features in turbulent and transitional boundary layers. In Fluid Mechanics of Internal Flow (ed. G. Sovran), pp. 2779. Elsevier.
Kline, S. J. & Mcclintock, F. A. 1953 Describing uncertainties in single-sample experiments Mech. Engng 75, 38.Google Scholar
Kline, S. J., Reynolds, W. C., Schraub, F. A. & Runstadler, P. W. 1967 The structure of turbulent boundary layers J. Fluid Mech. 30, 741773.Google Scholar
Launder, B. E. & Jones, W. P. 1969 Sink flow turbulent boundary layers J. Fluid Mech. 38, 817831.Google Scholar
Launder, B. E. & Stinchcombe, H. S. 1967 Non-normal similar turbulent boundary layers. Imperial Coll. Mech. Engng Tech. Rep. TWF/TN 21.Google Scholar
Mceligot, D. M. 1963 The effect of large temperature gradients on turbulent flow of gases in the downstream region of tubes. Ph.D. thesis, Stanford University, TID-19446.
Mceligot, D. M., Coon, C. W. & Perkins, H. C. 1970 Relaminarization in tubes Int. J. Heat Mass Transfer 13, 431433.Google Scholar
Mceligot, D. M., Ormand, L. W. & Perkins, H. C. 1966 Internal low Reynolds number turbulent and transitional gas flow with heat transfer. Trans. A.S.M.E. C: J. Heat Transfer 88, 239245.
Murphy, H. D. 1979 Flow near the outlet of a geothermal energy reservoir. Ph.D. thesis, University of Arizona. Also Report LA-7906-T, available from the National Technical Information Service.
Narasimha, R. & Sreenivasan, K. R. 1973 Relaminarization in highly accelerated turbulent boundary layers J. Fluid Mech. 61, 417447.Google Scholar
Narasimha, R. & Sreenivasan, K. R. 1979 Relaminarization of fluid flows Adv. Appl. Mech. 19, 221309.Google Scholar
Patel, V. C. 1965 Calibration of the Preston tube and limitations on its use in pressure gradients J. Fluid Mech. 23, 185208.Google Scholar
Patel, V. C. & Head, M. R. 1968 Reversion of turbulent to laminar flow J. Fluid Mech. 34, 371392.Google Scholar
Shaw, R. 1960 The influence of hole dimensions on static pressure measurements J. Fluid Mech. 7, 550564.Google Scholar
Smits, A. J., Eaton, J. A. & Bradshaw, P. 1979 The response of a turbulent boundary layer to lateral divergence J. Fluid Mech. 94, 243268.Google Scholar
Worsoe-Schmidt, P. M. 1967 Heat transfer in the thermal entrance region of circular tubes and annular passages with fully developed laminar flow Int. J. Heat Mass Transfer 10, 541551.Google Scholar