Lagrangian and spectral analysis of the forced flow past a circular cylinder using pulsed tangential jets

Nicolaenko, Shock wave solutions of the Boltzmann equation as a nonlinear bifurcation problem from the essential spectrum, in: Th´ eories cin´ etiques classiques et

However, for the rotating- disk flow there is no free stream flow outside the boundary layer (apart from a weak axial flow component): the only known speed is the speed of rotation

For the three-dimensional boundary layer produced by a rotating disk, the scenario leading from the unperturbed boundary layer to the tur- bulent state takes place in two steps

Effects of nozzle-exit boundary-layer profile on the initial shear- layer instability, flow field and noise of subsonic jets.7. Effects of nozzle-exit

Existence for Euler and Prandtl equations. Construction of the Navier-Stokes solution. Swann, The convergence with vanishing viscosity of non-stationary Navier-Stokes flow to ideal

We connect this instability with the dynamics of corner vortices adjacent to the tip of the ellipse by observing that the typical turnover time of the corner vortex matches the

Abbreviations : AACE, American Association of Clinical Endocrinologists ; AMPK, Adenosine Monophosphate-Activated Protein Kinase ; CC, Cardiovascular Continuum ; CK, Creatin

When such particles were applied to tooth enamel samples in concentrations corresponding to the fluoride content of typical mouth rinses or toothpastes, they interacted with