2000
DOI: 10.1007/978-3-662-05902-9_1
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Fast Beams, Production and Detection

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Cited by 13 publications
(20 citation statements)
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“…In a free-jet, the gas reaches its limit velocity v ∞ very rapidly downstream from the nozzle, i.e., after covering a distance equivalent to only a few slit widths. The limit velocity corresponds to a complete conversion of the enthalpy of the gas into kinetic energy (Mach number M → ∞; flow temperature T → 0 K), and it is then easily retrieved from the conservation of energy equation, v ∞ = (2 c p T 0 ) 1/2 , where c p is the heat capacity at constant pressure of the carrier gas and T 0 is the stagnation temperature, fixed at 313 K in the present study. The value obtained for a flow of argon is 570 m/s, which is remarkably close to the value of 558 m/s calculated from the Mach number and the temperature extracted from the Pitot probe measurement ( v = aM , where is the speed of sound, γ is the specific heat ratio, and r is the specific gas constant), thus validating the T → 0 K approximation.…”
Section: Experimental Setup and Recording Of The Spectramentioning
confidence: 99%
“…In a free-jet, the gas reaches its limit velocity v ∞ very rapidly downstream from the nozzle, i.e., after covering a distance equivalent to only a few slit widths. The limit velocity corresponds to a complete conversion of the enthalpy of the gas into kinetic energy (Mach number M → ∞; flow temperature T → 0 K), and it is then easily retrieved from the conservation of energy equation, v ∞ = (2 c p T 0 ) 1/2 , where c p is the heat capacity at constant pressure of the carrier gas and T 0 is the stagnation temperature, fixed at 313 K in the present study. The value obtained for a flow of argon is 570 m/s, which is remarkably close to the value of 558 m/s calculated from the Mach number and the temperature extracted from the Pitot probe measurement ( v = aM , where is the speed of sound, γ is the specific heat ratio, and r is the specific gas constant), thus validating the T → 0 K approximation.…”
Section: Experimental Setup and Recording Of The Spectramentioning
confidence: 99%
“…This estimation does not represent satisfactorily the data as shown in Section 4. In the second way, the estimation of the perpendicular temperature is calculated approximating the gas expansion by a continuum expansion in which the temperature scales with the distance r from the source as T normalC ( r ) = 0.287 · T normalo r 4 / 3 where T o is the source temperature. Assuming the same distance for the quitting surface as in the first way, the final temperature at the quitting surface can be calculated as T C * = T C ( D QS ).…”
Section: Theoretical Modelmentioning
confidence: 99%
“…Low (thermal) energy, neutral atom and molecule beams are important in several fields of science and applied research. They are employed for example in high energy physics for jet target experiments, in experiments on molecular interaction, in spectroscopic studies of fragile species, , and in the investigation of matter wave properties and quantum coherence. …”
Section: Introductionmentioning
confidence: 99%
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