AIAA Journal · 1974 · 15 citations · 19 references
Natural SciencesAerospace EngineeringPhysicsAerodynamicsFluid DynamicsFluid MechanicsBoundary Layer MixingTurbulenceTurbulent FlowTurbulent MixingTurbulent TransportViscous FlowFree Shear FlowsFree-shear TurbulenceMach NumberMach Number EffectsShear StressTurbulent Kinetic EnergyTurbulent Mixing Length ScalesVelocity
The applicability of Bradshaw's interaction hypothesis to two-dimensional free shear flows was investigated. According to it, flows with velocity extrema may be considered to consist of several interacting layers. The hypothesis leads to a new expression for the shear stress which removes the usual restriction that shear stress vanishes at the velocity extremum. The approach is based on kinetic energy and the length scale equations. The compressible flow equations are simplified by restriction to low Mach numbers, and the range of their applicability is discussed. The empirical functions of the turbulence model are found here to be correlated with the spreading rate of the shear layer. The analysis demonstrates that the interaction hypothesis is a workable concept.
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The structure of turbulent shear flow
Journal of the Franklin Institute · 1956 · 3.8K citations
The structure of a self-preserving turbulent plane jet
L. J. S. Bradbury · Journal of Fluid Mechanics · 1965 · 495 citations