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  • 1970-1974  (3)
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  • 1
    Publication Date: 1973-12-18
    Description: The boundary-layer flow over a circular cylinder at a Reynolds number of 1·06 × 105 has been studied both experimentally and theoretically. The investigation was designed to concentrate on the self-induced oscillations occurring in the flow; at this Reynolds number, these oscillations have generally been ignored heretofore. In the experimental part of the investigation both the inviscid flow and boundary-layer flow reversals were measured as functions of time. The theoretical part of the study started with the measured inviscid flow and calculated all the boundary-layer characteristics. The boundary-layer calculations themselves revealed some very interesting fine-scale structure of the flow, which strongly indicated that the vanishing of wall shear does not signal the onset of separation for unsteady flow. In general, the agreement between the theoretical calculations and the experimental results was excellent and the unsteady component of this supposedly steady flow was found to be very significant. © 1973, Cambridge University Press. All rights reserved.
    Print ISSN: 0022-1120
    Electronic ISSN: 1469-7645
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics , Physics
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  • 2
    Publication Date: 2019-07-13
    Description: It is shown that three-dimensional and time-dependent boundary layer flows can be calculated in a reasonable amount of time with the current generation of computers. The physical problems used to illustrate this have a wide application, and are the following: (1) oscillating flows over cylinders with both the wall and the inviscid flow oscillating, and (2) time-dependent and three-dimensional flow over a rotating airfoil in forward flight.
    Keywords: FLUID MECHANICS
    Type: International Conference on Numerical Methods in Fluid Mechanics; Jul 03, 1972 - Jul 07, 1972; Paris; France
    Format: text
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  • 3
    Publication Date: 2019-07-13
    Description: Retreating blade stall experiments on model helicopter rotor, considering series of pressure distribution and boundary layer events
    Keywords: AERODYNAMICS
    Type: AHS PREPRINT 521 , ANNUAL NATIONAL V/STOL FORUM; May 19, 1971 - May 21, 1971; WASHINGTON, DC
    Format: text
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