Some observations of the transition process on the windward face of a long yawed cylinder
- 1 January 1985
- journal article
- research article
- Published by Cambridge University Press (CUP) in Journal of Fluid Mechanics
- Vol. 150, 329-356
- https://doi.org/10.1017/s0022112085000155
Abstract
An experiment has been performed to determine the effect of yaw upon transition in the boundary layer formed on the windward face of a long cylinder. The china-clay-evaporation and surface-oil-flow techniques have been used to study the development of the fixed-wavelength stationary disturbances which are characteristic of cross-flow instability. It has been found that the boundary layer is also susceptible to time-dependent disturbances which grow to very large amplitudes prior to the onset of transition. These disturbances have been studied with a hot-wire anemometer. The conditions necessary for the onset and completion of transition have been determined by the use of surface Pitot tubes. Data from the experiment have been compared with the simple criteria for instability and transition which were proposed by Owen & Randall over thirty years ago. In general it has been found that these criteria are inadequate, and, where possible, improvements have been proposed. The raw data are presented in sufficient detail for them to be used to test, or calibrate, future theoretical models of the transition process in three-dimensional boundary-layer flows.Keywords
This publication has 6 references indexed in Scilit:
- Transition in the Infinite Swept Attachment Line Boundary LayerAeronautical Quarterly, 1979
- The Calculation of the Three-Dimensional Turbulent Boundary Layer: Part III. Comparison of Attachment-Line Calculations with ExperimentAeronautical Quarterly, 1969
- On the Flow Along Swept Leading EdgesAeronautical Quarterly, 1967
- The three-dimensional nature of boundary-layer instabilityJournal of Fluid Mechanics, 1962
- A Method of Wind-Tunnel Testing Through the Transonic RangeJournal of the Aeronautical Sciences, 1948
- Laminar Boundary-Layer Oscillations and Stability of Laminar FlowJournal of the Aeronautical Sciences, 1947