Some fleynolds number effects on a three-dimensional turbulent boundary layer

37th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1999, Pages

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

^a State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; DELTA WING AIRCRAFT; DOPPLER EFFECT; LASER DOPPLER VELOCIMETERS; REYNOLDS NUMBER; TURBULENCE;

BOUNDARY LAYER THICKNESS; FREE-STREAM SPEED; MOMENTUM THICKNESS; REYNOLDS NUMBER EFFECT; THREE-DIMENSIONAL TURBULENT BOUNDARY LAYER; THREEDIMENSIONAL (3-D); TURBULENCE STRUCTURES; TURBULENT BOUNDARY LAYERS;

ATMOSPHERIC THERMODYNAMICS;

EID: 84983127183     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

1. Ciochetto, D.S. and Simpson, R. L., 1997, "Analysis of Three-Dimensional Turbulent Shear Flow Experiments with Respect to Algebraic Modeling Parameters" Report VPI-AOE-248, submitted to DTIC.
2. Femholz, H.H., Krause, E., Nockemann, M., Schober, M., 1995, "Comparative measurement in the canonical boundary layer at Re0 s6 X 104 on the wall of the German-Dutch windtunnel", Physics of Fluids, 7, (6), pp. 1275-1281.
3. Ölçmen, M.S., 1990, An experimental study of a three-dimensional pressure-driven turbulent boundary layer, Ph.D. Dissertation, Virginia Tech; VPI-AOE-178; DTIC: ADA2294957XSP.
4. Ölçmen, 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, pp. 487-495.
5. Ölçmen, 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, pp. 225-262.
6. Ölçmen, 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, pp. 702-716.
7. Ölçmen, M.S., Simpson, R.L., and George, J. 1999 "Experimental Study of High Reynolds Number (Re0 = 23000) Two and Three-Dimensional Turbulent Boundary Layers" AIAA-99-0553, 37th Aerospace Sciences Meeting & Exhibit, Jan 11-14, Reno, NV.
8. Ölçmen, M.S., Simpson, R.L., George, J and Whitfield, C.C., 1998, "Experimental Study of High Reynolds Number (Re„ = 23000) Two and T hree-Dimensional Turbulent Boundary Layers" Report VPI-AOE-260, submitted to DTIC.
9. Simpson, R.L., 1996, "Aspects of Turbulent Boundary Layer Separation", Progress in Aerospace Sciences" Vol. 32, pp.457-521, 1996.