Übersetzung für "Wirbelschleppe" in Englisch

The more powerful air jets penetrate the main flow and generate severe turbulence and a turbulent wake.

The flow condition within the eddy wake is very turbulent.

A disruption arises for example due to a wake flow or wake turbulence of further wind turbines.

Do not collect the flotsam and jetsam that another leaves in his wake.

The content of your life is the love you leave in your wake.

It only leaves itself in its wake.

If the aircraft produces a weaker vortex, the breakup will sound like tearing a piece of paper.

The maximal tangential speed in the vortex may be derived from the position of the high-frequency flank.

Vortices coming closer to the LD-anemometer are traced by manually controlled distance reduction.

The schematically illustrated boundary 3 b of the horseshoe eddy and wake should not be seen as a sharply defined demarcation.

In this case it is also possible for the aircraft to directly encounter the wake vortex.

The C-pillars in the rear strongly face inwards, which clearly reduces the wake turbulence.

At the same time, there was also the attempt to accelerate the breakdown of the wake vortex by periodic aileron movements.

All the birds except the first fly in the upwash from the wingtip vortices of the bird ahead.

At this speed, the wake turbulence passing off the tail of the train, it's gonna run just north of level, right?

Now, if the vortex again reaches the scanning volume, it is now traced by increasing the distance until the vortex has been dissipated.

As soon as a vortex enters the scanning volume, the wind peak becomes smaller or disappears, and a complex signal structure appears.

On this plane, a sufficient height between the surface and vortex to be expected is covered by rapid elevation scanning.

Such diameter increase in the flow channel causes turbulence and flow separation and an increase of the vortex trail triggered by a velocity jump at the guide vanes.

The dispersion and the velocity of a complete or partial discharge of the supplied air can be improved still further by causing the aeration face and thereby the wing face to rotate about the center of gravity and to transfer the air into a divergent vortex trail.

Due to the polygonal shape of the housing wall, the gap between the guide vanes and the barrel face may be kept relatively small when the guide vanes are in their completely open condition; however, considerably large gaps appear both at the leading edge and the trailing edge when the vanes are slightly rotated in the direction towards the closed position, as is usual in normal operating conditions, the gaps causing a turbulence of the flow which causes a vortex trail which cannot be suppressed before it reaches the adjacent compressor.

With the disclosed bearing of the guide vanes, there results a flush extension for the area between the axis of rotation and the trailing edge of the vane between the guide vane and the barrel face of the spherical section, so that there is no turbulence at the trailing edge of the vane which continues in the form of a vortex trail.

The necessarily appearing small gap at the vane leading edge causes a turbulence; however, its vortex trail is suppressed within the nozzle-like extending spherical section due to the acceleration of the flow.

The operation of the vortex flowmeter is based on the fact that when medium flows on to the damming member, vortices are alternately induced on both sides of its end face and that the vortices form the so-called Karman vortex trail.

This increase in diameter in the flow channel leads to a burbling and to an increase in the trailing vortex caused by the discontinuity in speed at the guide vanes.

If the mass and concentration of the chemically active component of the chemical flow line indicators are held constant while their geometry is retained, then, for laminar flow, the form of the vortex or eddy trail with respect to its length and width is a measure of the boundary layer flow velocity and the degree of turbulence.

For this, the wake vortex produced by ATTAS was measured by LIDAR (Light Detection and Ranging) systems either stationed on the ground or installed in an aircraft.