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Experimental study of the stability of heated laminar boundary layers in water

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TLDR
In this paper, a low turbulence water tunnel with free-stream turbulence intensities of 0[sdot ]1-0[dot ]2 was used for temperature-compensated hot-film anemometry, and the experimentally observed increase in the minimum critical Reynolds number with increased wall heating agrees with the trend predicted by theory.
Abstract
Linear sinusoidal disturbances are introduced into the boundary layer over a heated flat plate of uniform surface temperature using a vibrating ribbon. The experiment is performed in a low turbulence water tunnel with free-stream turbulence intensities of 0[sdot ]1–0[sdot ]2%. Measurements are made using temperature-compensated hot-film anemometry. Neutral-stability characteristics obtained for the unheated case agree favourably with previous results obtained both in water and in air. Neutral-stability and spatial disturbance-growth-rate characteristics measured for wall temperatures up to 8°F above the free-stream temperature verify trends established by parallel-flow solutions of the disturbance momentum and energy equations. Disturbance growth rates and the band of amplified disturbance frequencies both decrease as wall heating is increased. The experimentally observed increase in the minimum critical Reynolds number Re c min with increased wall heating agrees with the trend predicted by theory. However, effects of non-parallel flow act to reduce the measured values of Re c min by about 120 units compared with predicted parallel-flow values independent of the level of wall heating.

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Citations
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Journal ArticleDOI

Physical mechanisms of laminar-boundary-layer transition

TL;DR: The physical mechanisms of the transition phenomenon depend extensively on the specific type of flow and the character of environmental disturbances as mentioned in this paper, which has attracted the attention of investigators for more than a century.
Journal ArticleDOI

Passive control of transition in three-dimensional boundary layers, with emphasis on discrete roughness elements.

TL;DR: In this paper, a brief review of laminar flow control techniques is given and a strategy for achieving Laminarization for transonic transport aircraft is discussed, and a review of some flight-test results on swept-wing transition is presented.
Book ChapterDOI

Dialogue on Progress and Issues in Stability and Transition Research

TL;DR: In this paper, the authors have carried on a dialogue on the nature of transition for over thirty-three years, focusing on observations and views on transition issues focusing principally on developments since the First IUTAM Symposium on Laminar-Turbulent Transition of 1979.
Journal ArticleDOI

Stability of free-convection flows of variable-viscosity fluids in vertical and inclined slots

TL;DR: In this paper, the stability of the buoyancy-driven parallel shear flow of a variable-viscosity Newtonian fluid between vertical or inclined plates maintained at different temperatures is studied theoretically.
Journal ArticleDOI

The effect of wall heating on instability of channel flow

TL;DR: In this paper, the effect of wall heating or cooling on the linear, transient and secondary growth of instability in channel flow is investigated. But the authors focus on the effects of the wall heating on channel flow.
References
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Journal ArticleDOI

On the effects of boundary-layer growth on flow stability

TL;DR: In this paper, the stability of small travelling-wave disturbances in the flow over a flat plate is discussed and an iterative method is used to generate an asymptotic series solution in inverse powers of the Reynolds number Rx = Ux/v to the power one half.
Journal ArticleDOI

Nonparallel stability of boundary‐layer flows

TL;DR: In this article, the spatial stability of two-dimensional incompressible boundary layer flows is analyzed using the method of multiple scales, taking into account the streamwise variations of the mean flow, the disturbance amplitude, and the wavenumber.
Journal ArticleDOI

The flat plate boundary layer. Part 1. Numerical integration of the Orr–-Sommerfeld equation

TL;DR: In this paper, numerical space-amplified solutions of the Orr-Sommerfeld equation for the case of a boundary layer on a flat plate have been calculated for a wide range of values of frequency and Reynolds number.
Journal ArticleDOI

The flat plate boundary layer. Part 3. Comparison of theory with experiment

TL;DR: In this article, a study of Tollmien-Schlichting waves in the Blasius boundary layer has been carried out under good flow conditions, where the maximum r.m.s. amplitude of u, the downstream component of perturbation velocity, was limited to about 0·06% of U0, the free-stream velocity.
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