Explore Books on
boundary layer separation

Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations

By David A. Boger

Control of low-speed turbulent separated flow over a backward-facing ramp

By John C. Lin

Numerical solutions of the complete Navier-Stokes equations

By H. A. Hassan

Enhanced design of turbo-jet LPT by separation control using phased plasma actuators

By Thomas C. Corke

Control of unsteady separated flow associated with the dynamic stall of airfoils

By Michael C. Wilder

Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction

By David S. Dolling

Computation of Navier-Stokes equations for three-dimensional flow separation

By Ching-Mao Hung

Unsteady three-dimensional marginal separation, including breakdown

By Peter W. Duck

3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

By Masashi Mizukami

Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil

By Dale Ashby

3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

By M. Mizukami

Experimental study of boundary layer behavior in a simulated low pressure turbine

By Rickey J. Shyne

Low speed analysis of mission adaptive flaps on a high speed civil transport configuration

By Victor R. Lessard

Control of flow separation and mixing by aerodynamic excitation

By Edward J. Rice

Stability of separating subsonic boundary layers

By Jamal A. Masad

Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method

By Euromech Colloquium (349th 1996 Göttingen, Germany)

Demonstration of separation delay with glow-discharge plasma actuators

By Lennart S. Hultgren

The three dimensional flow field at the exit of an axial-flow turbine rotor

By B. Lakshminarayana

Computation of three-dimensional boundary layers including separation

By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

Special course on three-dimensional supersonic/hypersonic flows including separation

By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

Vortex flow aerodynamics

By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

Calculation of 3D separated turbulent flows in boundary layer limit

By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

Flow separation in shock wave boundary layer interactions at hypersonic speeds

By A. Hamed

Effect of acoustic excitation on stalled flows over an airfoil

By K. B. M. O. Zaman