Physical evidence on stall inception from visual studies, mean-velocity-profile correlations, shear measurements, and fluctuations in separating boundary layers in the neighborhood of stall are discussed. Direct visual studies suggest that stall inception in the laminar boundary layer follows the classical model, but does not necessarily do so in the turbulent shear layer. It is useful to describe stall as a certain type of transition region, which can be long or short. Adoption of these ideas is shown to lead to better correlation of stall data and more complete understanding of available physical evidence. However, physical data on the relation between the various types of evidence in the turbulent case and their respective connections with the events in the transition region leading to stall are not presently complete. This suggests experiments of a certain type which should lead to further clarification of the process of stall inception in the turbulent boundary layer.
Skip Nav Destination
Article navigation
September 1961
This article was originally published in
Journal of Basic Engineering
Research Papers
Flow Models in Boundary-Layer Stall Inception
V. A. Sandborn,
V. A. Sandborn
Lewis Research Center, NASA, Cleveland, Ohio
Search for other works by this author on:
S. J. Kline
S. J. Kline
Stanford University, Stanford, Calif.
Search for other works by this author on:
V. A. Sandborn
Lewis Research Center, NASA, Cleveland, Ohio
S. J. Kline
Stanford University, Stanford, Calif.
J. Basic Eng. Sep 1961, 83(3): 317-327 (11 pages)
Published Online: September 1, 1961
Article history
Received:
August 1, 1960
Online:
November 3, 2011
Citation
Sandborn, V. A., and Kline, S. J. (September 1, 1961). "Flow Models in Boundary-Layer Stall Inception." ASME. J. Basic Eng. September 1961; 83(3): 317–327. https://doi.org/10.1115/1.3658953
Download citation file:
79
Views
Get Email Alerts
Cited By
Related Articles
On the Calculation of Length Scales for Turbulent Heat Transfer Correlation
J. Heat Transfer (October,2001)
Features of a Laminar Separated Boundary Layer Near the Leading-Edge of a Model Airfoil for Different Angles of Attack: An Experimental Study
J. Fluids Eng (February,2017)
Analysis of the Sutton Model for Aero-Optical Properties of Compressible Boundary Layers
J. Fluids Eng (March,2006)
LDA-Measurements of Transitional Flows Induced by a Square Rib
J. Fluids Eng (March,2002)
Related Proceedings Papers
Related Chapters
Cavitating Structures at Inception in Turbulent Shear Flow
Proceedings of the 10th International Symposium on Cavitation (CAV2018)
Extended Surfaces
Thermal Management of Microelectronic Equipment, Second Edition
Extended Surfaces
Thermal Management of Microelectronic Equipment