DTIC AD0660017: EXPERIMENTS ON TURBULENT BOUNDARY LAYERS pdf

DTIC AD0660017: EXPERIMENTS ON TURBULENT BOUNDARY LAYERS

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Description of the Book:

Experiments were conducted in a turbulent boundary layer near separation along a circular cylinder with the flow in the axial direction. The pressure gradient along the axis of the cylinder could be varied such that it was possible to maintain three boundary-layer configurations close to separation or with regions of reversed flow: (1) A turbulent boundary layer with skin friction zero; (2) A turbulent boundary layer with a separated region and reattachment further downstream with skin friction zero; (3) A turbulent boundary layer with a region of small but constant skin friction and normal separation. Pressure and skin friction along the cylinder wall, as well as mean velocity profiles in the boundary layer, were measured

• Creator/s: Defense Technical Information Center
• Date: 8/1/1967
• Year: 1967
• Book Topics/Themes: DTIC Archive, Fernholz, Hans, MASSACHUSETTS INST OF TECH CAMBRIDGE GAS TURBINE LAB, *CYLINDRICAL BODIES, *FLOW SEPARATION, *TURBULENT BOUNDARY LAYER, PRESSURE, SKIN FRICTION, VELOCITY

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