Abstract
Laser Doppler measurements and flow visualization are presented for a turbulent circular jet emerging into a low-velocity cross-stream and, then, impinging on a flat surface perpendicular to the jet-nozzle axis. The experiments were performed for a Reynolds number based on the jet-exit conditions of 6 × 104, a jet-to-crossflow velocity ratio of 30 and for an impingement height of 5 jet diameters and include mean and turbulent velocity characteristics along the two normal directions contained in planes parallel to the nozzle axis. The results, which have relevance to flows found beneath VSTOL aircraft in ground effect, show the presence of a complex 3-D scarf vortex formed around the impinging jet. In zones where measurement data are not available, the flow details are numerically-visualized using a solution of the finite difference form of the fully threedimensional Reynolds-averaged Navier-Stokes equations, incorporating the turbulence viscosity concept.
The turbulent structure of the flow is affected by flow distortion at the impinging zone, which results in an unconventional behaviour of the dimensionless structure parameters that determine the empirical constants in engineering models of turbulence. The relative magnitude of the terms involved in the transport equations for the turbulent stresses is quantified from the experimental data in order to assess the importance of these effects and show the extent to which the turbulent structure of the impingement zone is affected by extra rates of strain.
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Abbreviations
- D :
-
Diameter of jet
- H :
-
Height of crossflow tunnel
- k :
-
Turbulent kinetic energy
- R e :
-
Reynolds number
- R uv :
-
Shear stress correlation coefficient
- U :
-
Horizontal velocity component, U=Ū+u′
- V :
-
Vertical velocity component, V=V+v′
- X :
-
Horizontal coordinate
- Y :
-
Vertical coordinate
- Z :
-
Transverse coordinate
- v T :
-
Turbulent viscosity
- j :
-
Jet-exit value
- o :
-
Crossflow value
References
Adler, D.; Baron, A. 1979: Prediction of a three-dimensional circular turbulent jet in crossflow. AIAA J. 17, 168–174
Andreopoulos, J. 1985: On the structure of jets in a crossflow. J. Fluid Mech. 157, 163–197
Andreopoulos, J.; Rodi, W. 1984: Experimental investigation of jets in a crossflow. J. Fluid Mech. 138, 93–127
Araújo, S. R. B.; Durão, D. F. G.; Firmino, F. J. G. 1982: Jets impinging normally and obliquely to a wall. AGARD CP 308, paper 5
Barata, J. M. M. 1989: Experimental at numerical study of the aerodynamics of impinging jets in a crossflow. Ph.D. Thesis, Instituto Superior Técnico, Technical University of Lisboa (In Portuguese)
Barata, J. M. M., Dur~ao, D. F. G., Heitor, M. V. and McGuirk, J. J. 1991: The impingement of single and twin turbulent jets through a crossflow. AIAA J. 29 (4), 595–602
Barata, J. M. M., Dur~ao, D. F. G. and McGuirk, J. J. 1989: Numerical study of single impinging jets through a crossflow. J. Aircraft, 26 (11) 1002–1008
Bradshaw, P. 1973: Effects of streamline curvature on turbulent flow. Agardograph 169
Castro, I. P. and Bradshaw, P. 1976: The turbulence structure of a highly curved mixing layer. J. Fluid Mech. 73 (2) 265–304
Chandrsuda, C. and Bradshaw, P. 1981: Turbulence structure of a reattaching mixing layer. J. Fluid Mech. 110, 171–194
Childs, R. E. and Nixon, D. 1985: Simulation of impinging turbulent jets. Paper AIAA-85-0047 presented at the AIAA 23rd Aerospace Sciences Meeting, Jan. 14–17, Reno, Nevada
Crabb, D., Durão, D. F. G. and Whitelaw, J. H. 1981: A round jet normal to a crossflow. J. Fluids Engng. 103, 142–153
Demuren, A. O. 1983: Numerical calculations of steady three-dimensional turbulent jets in crossflow. Comp. Meth. in Appl. Mech. and Engng. 37, 309–328
Durão, D. F. G.; Laker, J. R. and Velho, A. 1985: Velocity and amplitude bias and the development of laser anemometry counters. ASME Winter Annual Meeting Miami Beach, Florida, Nov. 17–22. ASME FED vol. 33, 235–240
Durst, F.; Melling, A.; Whitelaw, J. H. 1981: Principles and Practice of Laser-Doppler Anemometry, 2nd ed. New York: Academic Press
George, W. K.; Taulbee, D. B. 1990: Designing experiments to test closure hipotheses. In: Engineering turbulence modelling and experiments (eds. Rodi, W.; Ganic, E. N.), New York: Elsevier 383–397
Harsha, P. T. and Lee, S. C. 1970: Correlation between shear stress and turbulent kinetic energy. AIAA J., 8, 1508–1510
Heitor, M. V.; Laker, J. R.; Taylor, A. M. K. P. and Vafidis, C. 1984: Introduction manual for the FS model 2 doppler-frequency counter. Imperial College of Science and Technology, Mech. Engng. Dept. Report FS/84/10
Jones, W. P. 1990: Turbulence modelling: current practice and future trends. Proc. Intl. Symp. on Engng. Turbulence Modelling and Measurements, Dubrovnick, Yugoslavia, Sept. 24–28
Jones, W. P. and McGuirk, J. J. 1980: Computation of a round turbulent jet discharging into a confined crossflow. In: “Turbulent Shear Flows-2”, eds. Bradbury et al., Springer Verlag, 223–245
Kamotani, Y. and Greber, I. 1974: Experiments on confined turbulent jets in a crossflow. NASA CR-2392
Keffer, J. F. and Baines, W. D. 1963: The round turbulent jet in a cross-wind. J. Fluid Mech. 15, 481–496
Launder, B. E. 1989: Second-moment closure: present ... and future? Intl. J. Heat Fluid Flow, 10, 282–300
Launder, B. E. and Spalding, D. B. 1974: The numerical computation of turbulent flows. Compt. Meths. Appl. Mech. Engng. 3, 269–289
Melling, A. and Whitelaw, J. H. 1975: Turbulent flow in a rectangular duct. J. Fluid Mech. 78, 285–315
Patankar, S. V., Basu, D. K. and Alpay, S. A. 1979: Prediction of the three-dimensional velocity field of a deflected jet. J. Fluids Engng. 99, 758–762
Ramsey, J. W. and Goldstein, R. J. 1972: Interaction of a heated jet with a deflecting stream. NASA CR 72613
Saripalli, K. R. 1983: Visualization Studies of jet impingement flows at McDonnell douglas research laboratories. In: “Flow Visualization III”, Proc. 3rd Int. Symp. on Flow Visualization, ed. W.J. Young, Univ. Michigan, Sept. 6–9
Shabaka, I. M. N. A. and Bradshaw, P. 1981: Turbulent flow measurements in an idealized wing body function, AIAA journal, 19, 131–139
Shayesteh, M. V.; Shabaka, I. M. N. A. and Bradshaw, P. 1985: Turbulent structure of a three-dimensional impinging jet in a Crossflow. Paper AIAA 85-0044, AIAA 23rd Aerospace Sciences Meeting, Reno-Nevada, 14–17
Stoy, R. C. and Ben-Haim, Y. 1973: Turbulent jets in a confined Crossflow. J. Fluids Engng. 95, 551–556
Sugiyama, Y. and Usami, Y. 1979: Experiments on the Flow in and around jets directed normal to a crossflow. Bulletin JSME, 22, 1736–1745
Taylor, A. M. K. P. and Whitelaw, J. M. 1984: Velocity Characteristics in the turbulent near wake flows of confined axysymmetric bluff bodies. J. Fluid Mech. 139, 391–416
Tennekes, H. and Lumley, J. L. 1972: A First Course in Turbulence. The MIT Press
Walker, J. D. A. 1978: The boundary layer due to rectilinear vortex. Proc. Royal Soc. London, A, 359, 167–188
Yanta, W. J. and Smith, R. A. 1978: Measurements of turbulent-transport properties with a laser-doppler velocimeter. AIAA paper 73-169, 11th Aerospace Science Meeting, Washington
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Barata, J.M.M., Durão, D.F.G., Heitor, M.V. et al. On the analysis of an impinging jet on ground effects. Experiments in Fluids 15, 117–129 (1993). https://doi.org/10.1007/BF00190951
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DOI: https://doi.org/10.1007/BF00190951