AIAA Journal · 1985 · 90 citations · 9 references
AeroacousticsEngineeringFluid MechanicsObserved Transition LocationWave MotionBoundary LayerCalculation SchemeStabilityUnsteady FlowNumerical SimulationBoundary Element MethodHydrodynamic StabilityThree-dimensional Boundary-layer StabilityFree Boundary ProblemDisturbance WavesAerospace EngineeringCivil EngineeringAerodynamicsVortex Induced Vibration
The problem of the stability of a three-dimensional laminar boundary layer formed on a curved surface is considered. A calculation scheme, which takes account of the curvature of the flow streamlines and of the surface is proposed for the prediction of the development of small amplitude temporal disturbances. Computations have been performed for the flow over the windward face of an infinitely long yawed cylinder and comparisons have been made with experimental data. These indicate that the theory correctly predicts many of the features of the unstable laminar flow. The theory also suggests that transition, in this particular situation, is dominated by traveling disturbance waves and that, at the experimentally observed transition location, the wave which has undergone greatest total amplification has an amplitude ratio of approximately e to the 11th. When the effects of curvature are omitted the maximum amplitude ratio at transition is about e to the 17th.
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Instability and transition in rotating disk flow
Mujeeb R. Malik, Stephen Wilkinson, Steven A. Orszag · AIAA Journal · 1981 · 227 citations
On Stability and Transition in Three-Dimensional Flows
Tuncer Cebeci, K. Stewartson · AIAA Journal · 1980 · 179 citations
Stability of Three-Dimensional Boundary Layers
Ali H. Nayfeh · AIAA Journal · 1980 · 153 citations
Numerical Analysis, Kinematic Wave Theory, Multiple Scales +15