Abstract
A mathematical model of a gasdynamic laser with parallel supersonic mixing of the components and its applications to the choice of the geometrical characteristics of the nozzle unit of honeycomb construction are presented.
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Abbreviations
- T:
-
static temperature
- u:
-
velocity
- P:
-
pressure
- μ:
-
molecular weight
- ei :
-
average number of vibrational quanta
- k:
-
amplification ratio for a weak signal
- I:
-
radiation intensity
- ξi :
-
molar fraction of the component in the mixture
- δ* :
-
displacement thickness
- r, d:
-
current radius and diameter of the nozzle
- θ:
-
angle of inclination of the generating profile of the nozzle and characteristic temperature
- h:
-
enthalpy
- G:
-
flow rate
- L:
-
characteristic length
- A/A*:
-
expansion ratio of the nozzle
- Tw :
-
wall temperature
- ¯Tw=¯Tw/To :
-
temperature factor
- η=E ∼a /E* :
-
nozzle efficiency
- E:
-
stored vibrational energy
- X=X/(ra1 + ra2):
-
dimensionless coordinate
- 1:
-
radiating gas stream
- 2:
-
exciting gas stream
- 0:
-
stagnation value
- a, *, ∼:
-
values at the cut of the nozzle, in its critical cross section, and beyond the compression shock in the cross section of the nozzle cut
Literature cited
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Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 47, No. 1, pp. 53–59, July, 1984.
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Boreisho, A.S., Lebedev, V.F., Lobachev, V.V. et al. Calculation of the characteristics of a mixing CO2 gasdynamic laser with a nozzle unit of honeycomb construction. Journal of Engineering Physics 47, 781–786 (1984). https://doi.org/10.1007/BF00832592
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DOI: https://doi.org/10.1007/BF00832592