TERMIUM Plus^®

Fiche 1,  Justifications,  Anglais

Record number: 1, Textual support number: 1 CONT

In either case, the plasma, thus generated, can completely engulf the vehicle and persist far into the wake, precluding normal communications(telemetry and beacon track).  1, fiche 1, Anglais, - beacon%20track

Fiche 1,  Justifications,  Français

Record number: 1, Textual support number: 1 CONT

Dans les deux cas, le plasma ainsi produit est capable d'entourer complètement l'engin et de se continuer loin dans le sillage, empêchant les communications normales (télémesure et émission de radiophare).  1, fiche 1, Français, - %C3%A9mission%20de%20radiophare

Fiche 1,  Justifications,  Espagnol

Fiche 2,  Justifications,  Anglais

Record number: 2, Textual support number: 1 DEF

A vortex wake model used to assess the performance of horizontal axis wind turbines by partitioning the flow field downstream of the rotor into three regions.  2, fiche 2, Anglais, - fast%20free%20wake%20method

Record number: 2, Textual support number: 1 CONT

Success of vortex theories in the performance analysis of horizontal axis wind turbines depends greatly upon accurate specification of the geometry of the vortex wake... An earlier wake model of helicopter rotors is extended for wind turbine applications, the fast free wake method(FFW). The FFW was accomplished by partitioning the flow field downstream of the rotor into three regions :(1) the near wake, modeled as a series of straight vortex lines;(2) the intermediate wake, modeled as a number of vortex rings; and(3) the far wake, taken to be a semi-infinite cylindrical wake.  3, fiche 2, Anglais, - fast%20free%20wake%20method

Fiche 2,  Justifications,  Français

Record number: 2, Textual support number: 1 DEF

Modèle utilisé pour déterminer le sillage tourbillonnaire des éoliennes à axe horizontal par la séparation en trois dimensions du champ d'écoulement en aval du rotor.  2, fiche 2, Français, - mod%C3%A8le%20de%20sillage%20en%20trois%20domaines

Fiche 2,  Justifications,  Espagnol

Fiche 3,  Justifications,  Anglais

Record number: 3, Textual support number: 1 DEF

In vortex theories, one of the three regions partitioning the flow field downstream of the rotor, modeled as a series of straight vortex lines.  2, fiche 3, Anglais, - near%20wake

Record number: 3, Textual support number: 1 CONT

Success of vortex theories in the performance analysis of horizontal axis wind turbines depends greatly upon accurate specification of the geometry of the vortex wake... An earlier wake model of helicopter rotors is extended for wind turbine applications, the fast free wake method(FFW). The FFW was accomplished by partitioning the flow field downstream of the rotor into three regions :(1) the near wake, modeled as a series of straight vortex lines;(2) the intermediate wake, modeled as a number of vortex rings; and(3) the far wake, taken to be a semi-infinite cylindrical wake.  1, fiche 3, Anglais, - near%20wake

Fiche 3,  Justifications,  Français

Record number: 3, Textual support number: 1 DEF

Dans la théorie des tourbillons, une des trois dimensions issues de la séparation du champ d'écoulement en aval du rotor, modélisée sous forme d'une série de lignes tourbillonnaires droites.  2, fiche 3, Français, - sillage%20proche

Fiche 3,  Justifications,  Espagnol

Fiche 4,  Justifications,  Anglais

Record number: 4, Textual support number: 1 DEF

In vortex theories, one of the three regions partitioning the flow field downstream of the rotor, modeled as a number of vortex rings.  2, fiche 4, Anglais, - intermediate%20wake

Record number: 4, Textual support number: 1 CONT

Success of vortex theories in the performance analysis of horizontal axis wind turbines depends greatly upon accurate specification of the geometry of the vortex wake... An earlier wake model of helicopter rotors is extended for wind turbine applications, the fast free wake method(FFW). The FFW was accomplished by partitioning the flow field downstream of the rotor into three regions :(1) the near wake, modeled as a series of straight vortex lines;(2) the intermediate wake, modeled as a number of vortex rings; and(3) the far wake, taken to be a semi-infinite cylindrical wake.  1, fiche 4, Anglais, - intermediate%20wake

Fiche 4,  Justifications,  Français

Record number: 4, Textual support number: 1 DEF

Dans la théorie des tourbillons, une des trois dimensions séparant le champ d'écoulement en aval du rotor, modélisée sous forme d'un certain nombre d'anneaux tourbillonnaires.  2, fiche 4, Français, - sillage%20interm%C3%A9diaire

Fiche 4,  Justifications,  Espagnol

Fiche 5,  Justifications,  Anglais

Record number: 5, Textual support number: 1 DEF

In vortex theories, one of the three regions partitioning the flow field downstream of the rotor, modeled as a semi-infinite cylindrical wake.  2, fiche 5, Anglais, - far%20wake

Record number: 5, Textual support number: 1 CONT

Success of vortex theories in the performance analysis of horizontal axis wind turbines depends greatly upon accurate specification of the geometry of the vortex wake... An earlier wake model of helicopter rotors is extended for wind turbine applications, the fast free wake method(FFW). The FFW was accomplished by partitioning the flow field downstream of the rotor into three regions :(1) the near wake, modeled as a series of straight vortex lines;(2) the intermediate wake, modeled as a number of vortex rings; and(3) the far wake, taken to be a semi-infinite cylindrical wake.  1, fiche 5, Anglais, - far%20wake

Fiche 5,  Justifications,  Français

Record number: 5, Textual support number: 1 DEF

Dans la théorie des tourbillons, une des trois dimensions issues de la séparation du champ d'écoulement en aval du rotor, modélisée sous forme d'un sillage cylindrique à demi infini.  2, fiche 5, Français, - sillage%20%C3%A9loign%C3%A9

Fiche 5,  Justifications,  Espagnol

Fiche 6,  Justifications,  Anglais

Record number: 6, Textual support number: 1 CONT

The Advanced Solid Rocket Motor(ASRM) program was originally developed to address safety concerns in the wake of the space shuttle Challenger disaster. In developing this program, numerous technological improvements were made in addition to safety improvements, which have made this rocket design far superior to even the Revised Solid Rocket Motor(RSRM).  2, fiche 6, Anglais, - advanced%20solid%20rocket%20motor

Fiche 6,  Justifications,  Français

Fiche 6,  Justifications,  Espagnol