Examples of 'aerodynamic surface' in a sentence
Meaning of "aerodynamic surface"
aerodynamic surface: This phrase refers to a surface or structure that is designed to reduce air resistance and improve the efficiency or performance of an object moving through the air, such as an aircraft or vehicle
How to use "aerodynamic surface" in a sentence
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aerodynamic surface
System for controlling a mobile aerodynamic surface of an aircraft.
The aerodynamic surface then becomes covered in ice very quickly.
I am not able to design an aerodynamic surface.
The problem of such aerodynamic surface icing is well known in the aviation industry.
Device for articulating a flap to an aircraft aerodynamic surface.
The assembly must provide an aerodynamic surface of good geometrical quality.
Blade tips of the fan conform to a portion of the interior aerodynamic surface.
The present invention relates to an aerodynamic surface pattern for a golf ball.
Each technique requires one or more elements to be bonded to the aerodynamic surface.
A generally continuous aerodynamic surface is a surface that has a generally continuous aerodynamic contour.
Hybrid control system for an aircraft aerodynamic surface.
To bring the aerodynamic surface 3 into the commanded position by slaving.
Said body has at least one aerodynamic surface.
For preference, said aerodynamic surface is formed by a profile piece positioned transversely to said channel.
The deformation method can be applied to an aerodynamic surface of a ship.
See also
Secondly, the classical aerodynamic surface has little actuation for the case.
A structural element for covering an elongate gap on an aerodynamic surface of an aircraft.
An external annular aerodynamic surface for linking up with the external surface of said nacelle ;.
The deformation method can be applied to an aerodynamic surface of a submarine.
The aerodynamic surface could also be comprised in engine air intakes, inlet channels etc.
The surface is comprised of at least one of an aerodynamic surface and a hydrodynamic surface.
The present invention relates to a device for articulating a flap to an aircraft aerodynamic surface.
The problem is often handled by fitting the aerodynamic surface with a Joule effect heater device.
The openings open into a fluid stream flowing with a velocity relative to the aerodynamic surface.
A leading-edge slat is an aerodynamic surface running spanwise just ahead of the wing leading edge.
Wind turbine blade with device for changing the aerodynamic surface or shape.
At the aerodynamic surface was reduced to this end the carriage 20 mm.
The present invention relates to a system for controlling a mobile aerodynamic surface of an aircraft.
The aerodynamic surface as claimed in claim 10, wherein said sensors measure pressures.
Heater mat for using the Joule effect to heat an aerodynamic surface.
Figure 7 shows an example of an aerodynamic surface 1 with non-integrated blanket solutions.
Figure 1 shows the trajectories of water droplets impacting on an aerodynamic surface.
Figure 7 shows an example of an aerodynamic surface 1 with this non-integrated blanket solution.
Conventionally, such features are introduced by bonding elements to the aerodynamic surface.
FIG . 1 is a cross-section through an aerodynamic surface fitted with a heater mat of the invention ;.
In addition, the connection elements do not protrude in relation to the aerodynamic surface.
Method for manufacturing an aerodynamic surface ( 1 ) for an aircraft, comprising the steps of,.
In some aircraft, the air intake may be defined by an aerodynamic surface curvature.
The panel has a convex aerodynamic surface 14 and a concave interior surface 15 stiffened by stringers 16.
Thus, continuity of the control of said aerodynamic surface is obtained.
In particular, electrohydrodynamic coupling can be used to accelerate air flow near an aerodynamic surface.
The device as claimed in claim 8, wherein said second aerodynamic surface is entirely fixed.
They are very long, veined and most importantly, their shape creates a perfect aerodynamic surface.
The device as claimed in claim 6, wherein said first aerodynamic surface is entirely fixed.
Still further, the solar panel of another embodiment may be deposited onto the aerodynamic surface.
To this end, according to the invention, the aircraft aerodynamic surface comprising,.
The present invention relates to a modular anti-icing / de-icing device for an aerodynamic surface.
Thus, the outer wall 49 has an aerodynamic surface.
The end-fitting according to claim 1, in which said body has at least one aerodynamic surface.
Modular anti-icing / de-icing device for an aerodynamic surface.
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