Sentence examples for boundary layer control and from inspiring English sources

This is particularly the case at higher MB concentrations where larger C values indicate a greater degree of boundary layer control and deviation from the intraparticle diffusion model.

Porous tubes or channels have been under considerable attention because of their various applications in biomedical engineering, design of filters, transpiration cooling boundary layer control, and gaseous diffusion.

In addition, the mechanisms of different drag reductions based on the boundary layer control and the potential applications in fluid engineering are discussed.

Also the flow in porous tubes or channels has been under considerable attention in recent years because of its various applications in biomedical engineering, transpiration cooling boundary layer control, and gaseous diffusion.

Consequently, flow and boundary layer control and adaptive wing technology may have revolutionary new benefits for take-off, landing and cruise operating conditions for many aircraft by enabling real-time effective geometry optimization relative to the flight conditions.

Two important approaches to alleviation of control chattering in sliding mode control are the boundary layer control (BLC) and the dynamic sliding mode control (DSMC).

The emphasis is placed on experimentation relating to hydrodynamic excitation, although acoustic methods as well as traditional boundary layer control, such as steady blowing and suction, are discussed in order to provide an appropriate historical context for recent developments.

This recirculating system requires no net mass bleed and therefore has advantages for boundary layer control in external or mixed-compression supersonic aircraft inlets.

Boundary layer control (BLC) for delta wing micro-aircraft increases the manoeuvrability and performance of the MAV.

In this paper, the various state-of-the-art approaches of drag-reducing and energy-saving technologies based on the boundary layer control are reviewed, focusing on the polymer drag reduction additives, the micro-morphology, the super-hydrophobic surface, the micro air bubbles, the heating wall, the vibrant flexible wall and the composite drag reduction methods.

To validate the effects described in Section Boundary Layer Control, a wind tunnel test was conducted for the belt-driven wing and the non-driven wing, both of which had the same airfoil shape.