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Calculation of the characteristics of a mixing CO2 gasdynamic laser with a nozzle unit of honeycomb construction

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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

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