John F. Foss

Springer handbook of experimental fluid mechanics

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Turbulent boundary layer to single-stream shear layer: the transition region

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Secondary Flow Effects in a Bounded Rectangular Jet

This communication presents the results and conclusions of an experimental study of the near-separation region of a single-stream shear layer. The momentum thickness at separation (

Statistical structure of turbulent-boundary-layer velocity–vorticity products at high and low Reynolds numbers

x\,{=}\,0

Near Exit Plane Effects Caused by Primary and Primary-Plus-Secondary Tabs

) was

The Measurement of Vorticity in Transitional and Fully Developed Turbulent Flows

\theta_0\,{=}\,9.6

Pulse width modulated constant temperature anemometer

mm, with Reynolds number

Hot-Wire Measurements Around a Controlled Diffusion Airfoil in an Open-Jet Anechoic Wind Tunnel

\hbox{\itshape Re}_\theta\,{=}\,4650

Measurements in a large angle oblique jet impingement flow

. Boundary layer separation was caused by a sharp

On the sign of the instantaneous spanwise vorticity component in the near‐wall region of turbulent boundary layers

90^{\circ}