Experimental study of high reynolds number (Reθ=23200) two and Three-Dimensional turbulent boundary layers

37th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1999, Pages

  Semih Olcmen M ^a   Simpson, Roger L ^a   George, Jacob ^a  

^a State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; ATMOSPHERIC THERMODYNAMICS; BOUNDARY LAYER FLOW; DOPPLER EFFECT; LASER DOPPLER VELOCIMETERS; REYNOLDS NUMBER; TURBULENCE; TURBULENT FLOW;

HIGH REYNOLDS NUMBER; MEAN VELOCITIES; MOMENTUM THICKNESS; PRESSURE-DRIVEN; REYNOLDS STRESS; SPATIAL RESOLUTION; THREE-DIMENSIONAL TURBULENT BOUNDARY LAYER; TURBULENT BOUNDARY LAYERS;

BOUNDARY LAYERS;

EID: 84983112840     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. AGARDOGRAPH 335, 1996, “Turbulent boundary layers in subsonic and supersonic flow”, AGARD, 7 Rue Ancelle, 92200 Neuilly-sur-Seine, France. Edited by Prof. William Saric, Arizona State University, Tempe, AZ 85287-610, USA.
2. Fernholz, H.H., and Finley, P.J., 1996, “The incompressible zero-pressure-gradient turbulent boundary layer: An assessment of the data”, Prog. Aerospace Sci, vol. 32, 245-311. Elsevier Science Ltd.
3. Fernholz, H.H., Krause, E., Nockemann, M., Schober, M., 1995, “Comparative measurement in the canonical boundary layer at ReB<6 X 104 on the wall of the German-Dutch windtunnel”, Physics of Fluids, 7, (6), 1275-1281.
4. Ligrani, P.M., and Bradshaw, P., 1987, “Spatial resolution and measurement of turbulence in the viscous sublayer using subminiature hot-wire probes.”, Experiments in Fluids, 5, 407-417.
5. Nockemann, M., Abstiens, R., Schober, M., Bruns, J., Eckert, D., 1994, “Messungen in einer turbulenten Wandgrenzschicht bei groften Reynolds-Zahlen im Deutsch_Niederlandischen Windkanal Mepbericht”, Aerodynamischen Institut report, der Rhein.-West… Technischen Hochschule Aachen, Germany, Professor: E. Krause, Ph. D.
6. Ölcmen, M.S., and Simpson, R.L, 1992, “Perspective: On the Near wall similarity of three-dimensional turbulent boundary layers”, Transactions of ASME, J. of Fluids Engineering., vol. 114, 487-495.
7. Ölcmen, M.S., and Simpson, R.L, 1995a, “An experimental study of a three-dimensional pressure-driven turbulent boundary layer”, J. of Fluid Mech., vol. 290, 225-262.
8. Ölcmen, M.S., and Simpson, R.L, 1995b, “A five-velocity-component laser-Doppler velocimeter for measurements of a three-dimensional turbulent boundary layer”, Meas. Sci. and Tech., vol. 6, 702-716.
9. Ölcmen, M.S., Simpson, R.L., George, J., and Whitfield, C.C., 1998, “Experimental Study of High Reynolds Number (ReB = 23000) Two and Three-Dimensional Turbulent Boundary Layers”, Report VPI-AOE-260, submitted to DTIC.
10. Ölcmen, M.S., Simpson, R.L., and George, J., 1999, “Some Reynolds Number Effects on a Three-dimensional Turbulent Boundary Layer,” AIAA-99-0554, 37th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Jan. 11-14.
11. Simpson, R.L., 1996, “Aspects of Turbulent Boundary Layer Separation”, Progress in Aerospace Sciences,” Vol. 32, 457-521, 1996.