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Proceedings ArticleDOI

The wave pattern produced by a point source on a rotating disk

L. M. Mack
TLDR
In this article, the wave pattern produced by a zero-frequency point source located at the Reynolds number of the artificial roughness element in an experiment conducted by Wilkinson and Malik (1983) was analyzed.
Abstract
It is pointed out that the boundary layer on a rotating disk is important in stability theory because it provides a particularly simple way to study the important phenomenon of crossflow instability. This type of instability is responsible for early transition on sweptback wings. Mack and Kendall (1983) have studied the wave patterns formed by harmonic point sources in a Blasius boundary layer on the basis that the source uniformly excites all oblique normal modes of the source frequency. The calculation procedure for planar boundary layers was modified to fit the different geometry of the rotating disk and the lack of an axis of symmetry. Calculations were performed of the wave pattern produced by a zero-frequency point source located at the Reynolds number of the artificial roughness element in an experiment conducted by Wilkinson and Malik (1983). The results provided in the present investigation confirm that the experimental wave pattern is a superposition of the complete azimuthal wavenumber spectrum of zero-frequency normal modes with uniform initial amplitude and phase.

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Journal ArticleDOI

Absolute instability of the boundary layer on a rotating disk

TL;DR: In this paper, the inviscid stability of the boundary-layer flow over a disk rotating in otherwise still fluid is analyzed and it is suggested that absolute instability may cause the onset of transition from laminar to turbulent flow.
Journal ArticleDOI

An experimental study of absolute instability of the rotating-disk boundary-layer flow

TL;DR: In this article, the results of experiments on unsteady disturbances in the boundary-layer flow over a disk rotating in otherwise still air are presented, where the flow was perturbed impulsively at a point corresponding to a Reynolds number R below the value at which transition from laminar to turbulent flow is observed.
Journal ArticleDOI

Effect of Isolated Micron-Sized Roughness on Transition in Swept-Wing Flows

TL;DR: In this article, boundary-layer transition-to-turbulence studies are conducted in the Arizona State University Unsteady Wind Tunnel on a 45-deg swept airfoil.
Journal ArticleDOI

Global behaviour corresponding to the absolute instability of the rotating-disc boundary layer

TL;DR: In this article, a study of the linear global behaviour corresponding to the absolute instability of the rotating-disc boundary layer is carried out, based on direct numerical simulations of the complete linearized Navier-Stokes equations obtained with the novel velocity-vorticity method described in Davies & Carpenter (2001).
Proceedings ArticleDOI

Effect of micron-sized roughness on transition in swept-wing flows

TL;DR: In this paper, boundary-layer transition-to-turbulence studies are conducted in the Arizona State University Unsteady Wind Tunnel on a 45-degree swept airfoil.
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