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GAS EXIT TEMPERATURE [4 fiches]

Fiche 1 2004-01-27

Anglais

Subject field(s)
  • Spacecraft
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.

Français

Domaine(s)
  • Engins spatiaux
DEF

Partie d'une tuyère de section croissante, en aval du col, où se produit la détente du gaz.

OBS

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

PHR

Partie supérieure du divergent.

Espagnol

Conserver la fiche 1

Fiche 2 1998-05-14

Anglais

Subject field(s)
  • Analytical Chemistry
CONT

Flame Emissivity Detector. Another detector based on monitoring a specific property of a flame, its emissivity, was developed by Grant, who mixed coal gas in constant proportions with the effluent from a chromatographic column; this coal gas/effluent mixture burned at a wide stainless steel jet. The emissivity of the flame, changing as the flame’s carbon content is varied, is measured with the aid of a metal reflector, glass condensing lens, and selenium photocell; these are held in place from each other at their proper optical distances .... For low background emissivity values, response is nonlinear. However, by controlling the coal gas flow rate to maintain emissivity between 0.60 and 0.80 mV, detector response is linear over a wide temperature range.

OBS

For the determination of combustible components of organic origin in gas chromatographic effluents, various principles of detection based on flame reactions have been utilized, namely, the hydrogen flame temperature, flame emissivity, and flame ionization detectors. In all reported systems, specific flame properties were monitored. Whereas Scott measured the flame temperature of the exit gas at a small jet and Grant the flame's emissivity by optical means, Mc William and Dewar and Harley et al. advanced new detection concepts based on the electrical or ionization properties of hydrogen/oxygen flames.

Français

Domaine(s)
  • Chimie analytique

Espagnol

Conserver la fiche 2

Fiche 3 1998-05-14

Anglais

Subject field(s)
  • Analytical Chemistry
CONT

For the determination of combustible components of organic origin in gas chromatographic effluents, various principles of detection based on flame reactions have been utilized, namely, the hydrogen flame temperature, flame emissivity, and flame ionization detectors. In all reported systems, specific flame properties were monitored. Whereas Scott measured the flame temperature of the exit gas at a small jet and Grant the flame's emissivity by optical means, Mc William and Dewar and Harley et al. advanced new detection concepts based on the electrical or ionization properties of hydrogen/oxygen flames.

Français

Domaine(s)
  • Chimie analytique
Terme(s)-clé(s)
  • détecteur à flamme

Espagnol

Conserver la fiche 3

Fiche 4 1986-06-26

Anglais

Subject field(s)
  • Air Pollution
  • Atmospheric Physics

Français

Domaine(s)
  • Pollution de l'air
  • Physique de l'atmosphère

Espagnol

Conserver la fiche 4

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