Universal equations of the laminar boundary layer on a rotating blade

1973 ◽  
Vol 6 (2) ◽  
pp. 251-259 ◽  
Author(s):  
V. V. Bogdanova
Keyword(s):  
Boundary Layer ◽  
Laminar Boundary Layer ◽  
Rotating Blade

The Laminar Boundary Layer on a Rotating Circular Arc Blade

1966 ◽  
Vol 88 (1) ◽  
pp. 111-120
Author(s):  
R. M. Halleen ◽  
J. P. Johnston ◽  
W. C. Reynolds
Keyword(s):  
Boundary Layer ◽  
Laminar Boundary Layer ◽  
Perturbation Technique ◽  
Approximate Solutions ◽  
Boundary Layer Separation ◽  
Primary Objective ◽  
Centrifugal Impeller ◽  
Pressure Gradients ◽  
Boundary Layer Problem ◽  
Rotating Blade

The primary objective was to develop an exact solution to the simplest possible laminar boundary-layer problem for a curved rotating blade. It was formulated initially so that the results might be used to illuminate some of the characteristics of boundary-layer behavior on centrifugal impeller blades. The solution was obtained by a perturbation technique and the results compared to existing approximate solutions and related exact solutions. A primary result shows that rotation itself may induce laminar boundary-layer separation on a blade trailing face in the absence of free-stream, longitudinal adverse pressure gradients. This result is then interpreted to show that such a separation may become important for impellers of low ReD = uˆtD/ν; i.e., when ReD ≤ 900.

Automatic control of laminar boundary-layer transition

AIAA Journal ◽  
1997 ◽  
Vol 35 ◽  
pp. 85-90
Author(s):  
P. A. Nelson ◽  
M. C. M. Wright ◽  
J.-L. Rioual
Keyword(s):  
Boundary Layer ◽  
Automatic Control ◽  
Laminar Boundary Layer ◽  
Boundary Layer Transition ◽  
Layer Transition
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