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Hermann Schlichting, Erich Truckenbrodt: Aerodynamik des Flugzeugs Springer, Berlin 1967; Hermann Schlichting, Klaus Gersten, Boundary Layer Theory, 8th ed. Springer-Verlag 2004, ISBN 81-8128-121-7; Hermann Schlichting, Klaus Gersten, Egon Krause, Herbert, jun. Oertel: Grenzschicht-Theorie Springer, Berlin 2006, ISBN 3-540-23004-1
The boundary layer thickness, , is the distance normal to the wall to a point where the flow velocity has essentially reached the 'asymptotic' velocity, .Prior to the development of the Moment Method, the lack of an obvious method of defining the boundary layer thickness led much of the flow community in the later half of the 1900s to adopt the location , denoted as and given by
This turbulent boundary layer thickness formula assumes 1) the flow is turbulent right from the start of the boundary layer and 2) the turbulent boundary layer behaves in a geometrically similar manner (i.e. the velocity profiles are geometrically similar along the flow in the x-direction, differing only by stretching factors in and (,) [5 ...
The boundary layer around a human hand, schlieren photograph. The boundary layer is the bright-green border, most visible on the back of the hand (click for high-res image). In physics and fluid mechanics, a boundary layer is the thin layer of fluid in the immediate vicinity of a bounding surface formed by
At this moderate free-stream turbulence level, he observed a velocity perturbation signal with a frequency under 12 Hz, much smaller than the usual Tollmien-Schlichting wave frequency. He also observed fluctuations in boundary layer thickness, which does not occur in low-turbulence free-stream flow. [2]
Turbulent boundary layers are more resistant to separation. The energy in a boundary layer may need to be increased to keep it attached to its surface. Fresh air can be introduced through slots or mixed in from above. The low momentum layer at the surface can be sucked away through a perforated surface or bled away when it is in a high pressure ...
Schlichting jet is a steady, laminar, round jet, emerging into a stationary fluid of the same kind with very high Reynolds number. The problem was formulated and solved by Hermann Schlichting in 1933, [ 1 ] who also formulated the corresponding planar Bickley jet problem in the same paper. [ 2 ]
The transformation transforms the equations of axisymmetric boundary layer with external velocity in terms of original variables,,, into the equations of plane boundary layer with external velocity ¯ in terms of the new variables ¯, ¯, ¯, ¯. The transformation is given by the formulas