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rotor sustentateur

lifting rotor

transport terrestre - iate.europa.eu

L'invention concerne une voilure (11) destinée à un combiné comprenant un rotor sustentateur.

A wing (11) for a compound helicopter having a lifting rotor comprises a plurality of wing elements (12) of which one wing element is rotatably mounted and in one position thereof the wing elements form a single continuous aerofoil.

transports aérien et spatial - wipo.int

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Studies of a flat wake rotor theoryA computer code was developed at Princeton University to calculate the velocity components in the flow field near a lifting rotor....

général - core.ac.uk - PDF: hdl.handle.net

Normal component of induced velocity in the vicinity of a lifting rotor with a nonuniform disk loading /...aircraft.Part 1 preseents a method for computing, from available calculations for uniform disk loading, the effect of nonuniform circularly symmetrical disk loading on the normal component of induced velocity in the vicinity of a lifting rotor....

PDF: www.hathitrust.org

Concepts for a theoretical and experimental study of lifting rotor random loads and vibrations. phase 6-a: effects of blade torsion, of blade flap bending flexibility and of rotor support flexibility on rotor stability and random responseThe effects of lifting rotor blade torsion, blade flap bending flexibility and rotor support flexibility on rotor stability and random response are described....

PDF: hdl.handle.net

The normal component of the induced velocity in the vicinity of a lifting rotor and some examples of its application /...plane.This paper presents a practical method for computing the approximate values of the normal component of the induced velocity at points in the flow field of a lifting rotor....

PDF: www.hathitrust.org

Generalized performance limits for propellers, windmills and lifting rotors with axes parallel to the undisturbed flowAuthor(s) subject terms: Propellers, axial trubines, windmills, lifting rotors, helicopters, fans, performance coefficients, performance limits, momentum theory of propellers, actuator disc, vortex ring state of lifting rotor, stability of...

PDF: archive.org