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Fiche 1,  Justifications,  Anglais

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A comparatively small vessel with powerful engines and constructed in such a way as to be able to manoeuvre easily for towage and/or to assist in salvage operations at sea.  5, fiche 1, Anglais, - tugboat

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Tugboats are needed to pull or push large ships in confined waters such as in a harbor area and docks, and they are also needed to tow large ships on long ocean voyages.... They are capable of firefighting and salvage duties and may carry large capacity pumps for these purposes. One important design characteristic of a tugboat is its hull form and propulsion system are designed both for a given free running speed and a high thrust at zero speed. Furthermore, its upper deck layout is dictated by the need to get close into a variety of vessels and by the need to keep the towing point above the longitudinal center of lateral pressure so that a lateral pull has a minimum effect on maneuverability.  6, fiche 1, Anglais, - tugboat

Record number: 1, Textual support number: 1 OBS

towboat; tow boat: Not to be confused with "pusher tug," which can also be referred to as a "towboat."  7, fiche 1, Anglais, - tugboat

Fiche 1,  Justifications,  Français

Record number: 1, Textual support number: 1 DEF

Bâtiment conçu pour déplacer d'un point à un autre des bâtiments de navigation dans un port, sur un fleuve, une rivière ou en mer.  3, fiche 1, Français, - remorqueur

Fiche 1,  Justifications,  Espagnol

Fiche 2,  Justifications,  Anglais

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A burn time during which thrust, pressure, and burning surface area decrease.  2, fiche 2, Anglais, - regressive%20burning

Fiche 2,  Justifications,  Français

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Combustion d'un bloc de propergol dont la forme permet d'obtenir une diminution continue de la surface de combustion et, partant, de la poussée.  1, fiche 2, Français, - combustion%20d%C3%A9croissante

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combustion décroissante : terme et définition publiés au Journal officiel de la République française le 6 juin 2014.  2, fiche 2, Français, - combustion%20d%C3%A9croissante

Fiche 2,  Justifications,  Espagnol

Fiche 3,  Justifications,  Anglais

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Rotating a blade along its longitudinal axis until its chord line is parallel to the wind.  3, fiche 3, Anglais, - blade%20feathering

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One method of controlling lift and torque on a wind turbine rotor [by] decreasing the area of blade surface exposed to the wind, feathering reduces thrust and stress on the rotor and tower when the rotor is at rest.  3, fiche 3, Anglais, - blade%20feathering

Fiche 3,  Justifications,  Français

Record number: 3, Textual support number: 1 DEF

[...] régulation par variation de calage de pale qui consiste à augmenter l'angle de calage des pales du rotor éolien, entraînant ainsi la diminution de l'angle d'incidence des pales et la diminution de la surface des pales balayées par le vent.  3, fiche 3, Français, - r%C3%A9gulation%20par%20mise%20en%20drapeau%20des%20pales

Fiche 3,  Justifications,  Espagnol

Fiche 4,  Justifications,  Anglais

Record number: 4, Textual support number: 1 DEF

A series of overlapping rock slices separated by steeply inclined subparallel reverse faults and bounded above and below by major low-angle thrust surfaces.  6, fiche 4, Anglais, - imbricate%20structure

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The central part of the Knob Lake Basin area has been highly deformed by doubly plunging isoclinal folds, with axes trending northwest, that are cut by steep easterly dipping thrust faults which give rise to a complex imbricate regional structure.  7, fiche 4, Anglais, - imbricate%20structure

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The arrangement is somewhat similar to a set of books leaning against one another on an incompletely filled shelf.  6, fiche 4, Anglais, - imbricate%20structure

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imbricate structure: term used at Natural Resources Canada - Earth Sciences Sector.  8, fiche 4, Anglais, - imbricate%20structure

Fiche 4,  Justifications,  Français

Record number: 4, Textual support number: 1 CONT

La partie centrale du bassin de Knob Lake est très déformée en plis isoclinaux à double plongement de direction nord-ouest; ces plis sont recoupés par d'abruptes failles de chevauchement à pendage est qui ont donné naissance à une structure régionale imbriquée et complexe.  5, fiche 4, Français, - structure%20imbriqu%C3%A9e

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structure imbriquée; structure en écailles : termes en usage à Ressources naturelles Canada - Secteur des sciences de la Terre.  6, fiche 4, Français, - structure%20imbriqu%C3%A9e

Fiche 4,  Justifications,  Espagnol

Fiche 5,  Justifications,  Anglais

Record number: 5, Textual support number: 1 CONT

A significant area of salt-cored compressional structures, thrust faults, and folds, as well as mobilized and deformed salt diapirs, occurs...  2, fiche 5, Anglais, - salt%2Dcored

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salt-cored: term used at Natural Resources Canada - Earth Sciences Sector.  3, fiche 5, Anglais, - salt%2Dcored

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Salt-cored anticline, diapir, fold, foldbelt, piercement structure.  3, fiche 5, Anglais, - salt%2Dcored

Fiche 5,  Justifications,  Français

Record number: 5, Textual support number: 1 CONT

Le terme de « diapir » est principalement réservé au contexte de couverture sédimentaire plissée, avec des plis à noyau salifère constitué de roches évaporitiques (gypse, anhydrite ou sel gemme).  2, fiche 5, Français, - %C3%A0%20noyau%20salif%C3%A8re

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à noyau salifère : terme en usage à Ressources naturelles Canada - Secteur des sciences de la Terre.  3, fiche 5, Français, - %C3%A0%20noyau%20salif%C3%A8re

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Anticlinal à noyau salifère.  4, fiche 5, Français, - %C3%A0%20noyau%20salif%C3%A8re

Fiche 5,  Justifications,  Espagnol

Fiche 6,  Justifications,  Anglais

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A type of stress-strain relationship occurring at the collision boundary of the North American and Pacific Plates in the Big Bend segment of the San Andreas Fault.  2, fiche 6, Anglais, - rotational%20compression

Record number: 6, Textual support number: 1 OBS

In very simple terms, this collision boundary is the San Andreas Fault Zone. In fact, the collision boundary is a much broader zone estimated to be a hundred kilometers in width near the project area. As the Pacific and North American Plates collide with each other, blocks of crust in each plate are thrust over or rotated with respect to other blocks.  2, fiche 6, Anglais, - rotational%20compression

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rotational compression: term used at Natural Resources Canada - Earth Sciences Sector.  3, fiche 6, Anglais, - rotational%20compression

Fiche 6,  Justifications,  Français

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compression rotationnelle; compression de rotation : termes en usage à Ressources naturelles Canada - Secteur des sciences de la Terre.  3, fiche 6, Français, - compression%20rotationnelle

Fiche 6,  Justifications,  Espagnol

Fiche 7,  Justifications,  Anglais

Record number: 7, Textual support number: 1 CONT

The solid rocket fuel fills the inside of the rocket from its top to the bottom. In the middle of the rocket is a shaped clearing that provides combustion area and allows the mixture to burn evenly. This shape may be a circle or a star depending upon the type of thrust desired for launch. The rocket's ignition commences by shooting flames down its entire length to initiate the combustion evenly throughout the grain, another term for solid rocket propellant. As the fuel burns and its waste parts are ejected out the nozzle the propellant area grows. As the propellant area grows there is more propellant to burn which means that the rocket's thrust increases.  2, fiche 7, Anglais, - combustion%20area

Fiche 7,  Justifications,  Français

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À l'intérieur de la chambre de combustion, zone où les ergols entrent en réaction.  2, fiche 7, Français, - foyer

Fiche 7,  Justifications,  Espagnol

Fiche 8,  Justifications,  Anglais

Record number: 8, Textual support number: 1 OBS

The central part of the Knob Lake Basin area has been highly deformed by doubly plunging isoclinal folds, with axes trending northwest, that are cut by steep easterly dipping thrust faults...  1, fiche 8, Anglais, - easterly%20dipping

Fiche 8,  Justifications,  Français

Record number: 8, Textual support number: 1 OBS

La partie centrale du bassin de Knob Lake est très déformée en plis isoclinaux à double plongement de direction nord-ouest; ces plis sont recoupés par d'abruptes failles de chevauchement à pendage est [...]  1, fiche 8, Français, - %C3%A0%20pendage%20est

Fiche 8,  Justifications,  Espagnol

Fiche 9,  Justifications,  Anglais

Record number: 9, Textual support number: 1 DEF

[A] cleaning method in which the detergent solution is forced through jets under high pressure into the carpet pile and immediately removed along with loose and emulsified soil through a wet vacuum.  1, fiche 9, Anglais, - steam%20cleaning

Record number: 9, Textual support number: 1 OBS

Many believe steam cleaning or hot water extraction is the best carpet cleaning method available... Hot water extraction utilizes a push-pull stroke for effective carpet cleaning. The hot water sprayer is located on the rear of the extraction wand. When the rearward thrust is made hot water is injected into the carpet pile where it is extracted a split second later by the extraction cup. The forward stroke is used to remove excess moisture and any remaining soil. For heavily soiled areas continuous back and forth motions can be used to increase the temperature of the area to assist in soil removal.  3, fiche 9, Anglais, - steam%20cleaning

Fiche 9,  Justifications,  Français

Record number: 9, Textual support number: 1 DEF

Méthode de nettoyage suivant laquelle la solution détergente est injectée sous forte pression dans le velours du tapis pour être immédiatement aspirée en même temps.  1, fiche 9, Français, - nettoyage%20par%20extraction

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Seul le nettoyage par extraction permet un nettoyage en profondeur.  3, fiche 9, Français, - nettoyage%20par%20extraction

Fiche 9,  Justifications,  Espagnol

Fiche 10,  Justifications,  Anglais

Record number: 10, Textual support number: 1 CONT

Solar Thermal Propulsion(STP)... uses large area deployable concentrators to focus the Sun's energy on a small heat exchanger, called an absorber, which is cooled by hydrogen gas propellant. The absorber transfers the concentrated heat energy from the Sun to the hydrogen gas. As the gas is heated, it expands and is directed outward through a nozzle. This expanding gas provides enough thrust in the microgravity environment of low earth orbit to transfer the vehicle to a higher energy, geosynchronous orbit around the Earth where the satellite operates.  2, fiche 10, Anglais, - solar%20thermal%20propulsion

Fiche 10,  Justifications,  Français

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Mode de propulsion solaire dans lequel l'énergie solaire sert à porter à haute température un agent propulsif.  2, fiche 10, Français, - propulsion%20h%C3%A9liothermique

Fiche 10,  Justifications,  Espagnol

Fiche 11,  Justifications,  Anglais

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In applying the principles of electrostrictive hydrodynamics(electrohydrodynamics) it is immediately clear to the aeronautical engineer that a large electrode area is required. Just as a sailboat uses a sail, any vehicle utilizing electrohydrodynamic propulsion must employ a large ballistic electrode to integrate the pressure of plasma "winds" to provide lift or forward thrust. These so-called "electric winds" are ion flows, moving at relatively high velocity. The flows may take various patterns determined by 1) The manner in which the flows are generated, and 2) The curvature of the surfaces which confine them.  1, fiche 11, Anglais, - electrohydrodynamic%20propulsion

Fiche 11,  Justifications,  Français

Fiche 11,  Justifications,  Espagnol

Fiche 12,  Justifications,  Anglais

Record number: 12, Textual support number: 1 CONT

A rocket engine is a device in which propellants are burned in a combustion chamber and the resulting high pressure gases are expanded through a specially shaped nozzle to produce thrust. The function of the nozzle is to convert the chemical-thermal energy generated in the combustion chamber into kinetic energy. The nozzle converts the slow moving, high pressure, high temperature gas in the combustion chamber into high velocity gas of lower pressure and temperature. Gas velocities from 2 to 4. 5 kilometers per second can be obtained in rocket nozzles. The nozzles which perform this feat are called DeLaval nozzles(after the inventor) and consist of a convergent and divergent section. The minimum flow area between the convergent and divergent section is called the nozzle throat. The flow area at the end of the divergent section is called the nozzle exit area.  6, fiche 12, Anglais, - divergent%20exit%20cone

Fiche 12,  Justifications,  Français

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Partie d'une tuyère de section croissante, en aval du col, où se produit la détente du gaz.  2, fiche 12, Français, - divergent

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Dans le divergent d'une tuyère à blocage sonique, la vitesse du gaz croît au-delà de la vitesse du son au col.  2, fiche 12, Français, - divergent

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Partie supérieure du divergent.  3, fiche 12, Français, - divergent

Fiche 12,  Justifications,  Espagnol

Fiche 13,  Justifications,  Anglais

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A stable area marginal to an orogenic belt, toward which the rocks of the belt were thrust or overfolded.  2, fiche 13, Anglais, - foreland

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The side of the range toward which the overturned folds incline is called the foreland ...  3, fiche 13, Anglais, - foreland

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Regional zoning occurs on a very large scale often corresponding to large sections of orogenic belts and their foreland ...  4, fiche 13, Anglais, - foreland

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Generally the foreland is a continental part of the crust, and is the edge of the craton or platform area.  2, fiche 13, Anglais, - foreland

Fiche 13,  Justifications,  Français

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Masse continentale demeurée stable vers laquelle la chaîne [de montagnes d'un géosynclinal] se trouve déversée [...]  3, fiche 13, Français, - avant%2Dpays

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Dans le concept de la tectonique des plaques, l'avant-pays représente l'ancienne marge stable, comme la bordure orientale du Massif central constitue l'avant-pays des Alpes.)  4, fiche 13, Français, - avant%2Dpays

Fiche 13,  Justifications,  Espagnol

Fiche 14,  Justifications,  Anglais

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... the Blended-Wing-Body(BWB) concept represents a potential revolution in subsonic transport.... In this study, 800 passenger BWB and conventional airplanes were compared for a 7000 nautical mile design range. ADP-class engines were used with technology levels keyed for a 2015 entry into service(EIS). In every measure, the BWB was found to be superior to the conventional configuration. Key findings for the BWB include : TOGW 15% lower[;] OEW 12% lower [;] Fuel-Burn 28% lower [;] Thrust 27% lower [;] L/D 21% higher [;] DOC 13% lower [. ] The BWB advantage results from a double-deck cabin that extends spanwise as well as lengthwise providing structural and aerodynamic overlap with the wing. This reduces the total wetted area of the airplane and the deep stiff centerbody provides efficient structural wingspan. Relaxed static stability allows optimal span loading, and a trailing-edge high-lift system is not required. Further synergy may be realized through buried engines that ingest the centerbody's boundary layer and thus reduce the effective ram drag.  2, fiche 14, Anglais, - blended%2Dwing%2Dbody%20project

Fiche 14,  Justifications,  Français

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Boeing en collaboration avec la NASA et trois universités américaines, a repris le projet BWB (Blended-Wing-Body) de McDonnell Douglas.  1, fiche 14, Français, - projet%20BWB

Fiche 14,  Justifications,  Espagnol

Fiche 15,  Justifications,  Anglais

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This adjustment is given in two ways : 1. With the patient in the neutral position, specific contact or contacts are taken on a vertebral process and the thrust is given in a specific direction... The thrust may be rapid with either a slow or fast release. 2. The adjustment is given by moving the patient in a specific direction to take out the active and passive motion at that level. The thrust is then given beyond the passive range of motion. It is possible to vary the velocity and depth or amplitude depending on the area being adjusted...  2, fiche 15, Anglais, - dynamic%20thrust

Fiche 15,  Justifications,  Français

Fiche 15,  Justifications,  Espagnol

Fiche 16,  Justifications,  Anglais

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The operating condition of a rotor when the axial flow through the rotor disk area is in the opposite direction to the axial flow outside the rotor disk area and to the rotor thrust.  1, fiche 16, Anglais, - vortex%2Dring%20state

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Term officialized by the ATSC - Helicopters.  2, fiche 16, Anglais, - vortex%2Dring%20state

Fiche 16,  Justifications,  Français

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Terme uniformisé par le CUTA - Hélicoptères.  1, fiche 16, Français, - %C3%A9tat%20de%20vortex

Fiche 16,  Justifications,  Espagnol

Fiche 17,  Justifications,  Anglais

Record number: 17, Textual support number: 1 CONT

Accurate control of the vertical flight profile(essentially thrust management) naturally enough yields the greatest savings; Lear Siegler puts these in the 2 to 7 per cent range, with perhaps 3. 5-4. 5 per cent representing the median area.  1, fiche 17, Anglais, - thrust%20management

Fiche 17,  Justifications,  Français

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C'est évidemment le contrôle précis du profil de vol vertical (c'est-à-dire la gestion de la poussée) qui assure les économies les plus importantes.  1, fiche 17, Français, - gestion%20de%20la%20pouss%C3%A9e

Fiche 17,  Justifications,  Espagnol

Fiche 18,  Justifications,  Anglais

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The coefficients used for moment are similar to coefficients of lift, drag, and thrust, and are likewise dimensionless; however, these must include a characteristic length, in addition to the area, the span is used for rolling or yawing moment, and the chord is used for pitching moment.  1, fiche 18, Anglais, - moment%20coefficient

Fiche 18,  Justifications,  Français

Record number: 18, Textual support number: 1 OBS

Il est égal à: (2 fois le moment) divisé par le produit de la masse volumique de l'air par la surface balayée, le carré de la vitesse du vent et le rayon du rotor.  2, fiche 18, Français, - coefficient%20de%20moment

Fiche 18,  Justifications,  Espagnol