Some observations of the transition process on the windward face of a long yawed cylinder

Author:

Poll D. I. A.

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.

Publisher

Cambridge University Press (CUP)

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference36 articles.

1. Owen, P. R. & Randall D. G. 1953 Boundary layer transition on a sweptback wing: a further investigation.RAE TM Aero 330.

2. Boltz F. W. , Kenyon, G. C. & Allen C. Q. 1960 Effects of sweep angle on the boundary layer stability characteristics of an untapered wing at low speeds.NASA TN D-338.

3. Owen, P. R. & Randall D. G. 1952 Boundary layer transition on a sweptback wing.RAE TM Aero 277.

4. Maltby, R. L. & Keating R. F. A. 1962 The surface oil flow technique for use in low speed wind tunnels.AGAR Dograph 70.

5. Anscombe, A. & Illingworth L. N. 1952 Wind-tunnel observations of boundary layer transition on a wing at various angles of sweep back. ARC R & M 2968.

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