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corde d'extrémité

tip chord

sciences naturelles et appliquées - iate.europa.eu

Pale de rotor principal incorporant une zone d'extrémité de pale de rotor présentant une corde d'extrémité et un cône d'extrémité, tels que le rapport de la corde de pale de rotor principal à la corde d'extrémité soit d'approximativement 0,30.

A main rotor blade incorporating a rotor blade tip region having a tip chord and a tip taper such that the ratio of the main rotor blade chord to the tip chord is approximately 0.30.

transports maritime et fluvial - wipo.int

Le site de fixation du générateur de tourbillons de type 'demi-soc' est défini en termes de longueur de la corde locale et de la corde d'extrémité.

The mounting site for the half-plow vortex generator is defined in terms of the length of the local and tip chords.

transports aérien et spatial - wipo.int

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Wind-tunnel investigation at mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control... The addition of the ram-air-jet spoiler tail fins or flow-through tip chord nacelles on the tail fins resulted in only small changes in basic missile longitudinal stability....

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

Ηp = propeller efficiency j = advance ratio... As a result, geometric characteristics of the flying wing such as span, tip chord and root chord are obtained....

PDF: enu.kz

Numerical analysis and geometry optimisation of vertical vane of room air-conditioner... The parameters investigated for optimisation of vertical vane are focused at length of long span, tip chord and short span....

PDF: doaj.org

Investigation in the langley 19-foot pressure tunnel of two wings of naca 65-210 and 64-210 airfoil sections with various type flaps /... Both wings had zero sweep, an aspect ratio of 9, and a ratio of root to tip chord of 2.5....

PDF: www.hathitrust.org

An experimental study of tip shape effects on the flutter of aft-swept, flat-plate wingsThe effects of tip chord orientation on wing flutter are investigated experimentally using six cantilever-mounted, flat-plate wing models....

PDF: hdl.handle.net