An analytical treatment of diffusion-type chemical lasers is presented. Chemical formation of the lasing molecule by laminar mixing and combustion of parallel streams of fuel and oxidizer is assumed to be diffusion controlled, and subsequent collisional deactivation of each vibrational level of the lasing molecule by nonreactive V -Kand V -T energy transfer is found by a successive-approximation scheme. Radiative processes are considered only for a downstream optical cavity of infinitesimal streamwise length. A laser employing the reaction H 2 + F -> HF(f) + H is considered in detail with the use of a single-boundary-layer, flame-sheet model. Expressions for integrated zero-power gain, laser power, and efficiency are obtained. It is found that the efficiency of conversion of chemical power (i.e., 3.15 Mw/lbm of F/sec) to laser radiant power is approximately 30 % when collisional deactivation is neglected in comparison with radiative deactivation. The effect of collisional deactivation is reduction of the efficiency to levels of 10 to 20 % for cases in which H 2 diffusion times are of the order of HF collisional deactivation times. In the latter regime, the efficiency varies approximately as [A>w(j; 6> _ e ) 1/2 ]~1. (p e is gas pressure, w is semiheight of the oxidizer channel, and y 6 _ e is the initial mass fraction of atomic fluorine.)
Nomenclaturec p = specific heat at constant pressure per unit mass D = binary diffusion coefficient / = nondimensional stream function, Eq. (11 a) G vJ = integrated gain coefficient, Eq. (38a) g = dimensionless total mixture enthalpy per unit mass g v j = optical gain coefficient, Eq. (37a) H = total mixture enthalpy per unit mass, Eq. (6) AH V = heat of reaction (per mole) appearing in excess relative translational and rotational energy of reaction products in Eqs. (0-3) of Table 1 h = Planck's constant; or static mixture enthalpy per unit mass /i? = heat of formation of i th species, Eq. (7) J = rotational quantum number k = thermal conductivity; or Boltzmann constant MJ.J 1 " 7 " 1 = matrix element of the electric-dipole moment, Table 3 N A = Avogadro's number P = available coherent power Pr = Prandtl number p = thermodynamic pressure R 0 = universal gas constant T = absolute translational temperature u, v = velocity components in the x and y directions, respectively v = vibrational quantum number W t = molecular weight of species i x,y = axial and transverse (optical) ordinates x c = axial location of cavity x c d9 x o -characteristic collisional-deactivation and diffusion distances, respectively, Eqs. (12) and (33b) y t = mass fraction of species i z v = probability of producing HF(t;) in Eqs. (0-3) of Table 1 a v = ratio of characteristic rotational temperature (in level v) to fuel temperature rj = boundary-layer similarity variable, Eq. (9); or chemicalto-stimulated-emission power-conversion efficiency v vj = frequency at center of P-branch line transition p = mass density \l/ = stream function Presented as Paper 71-28 at the AIAA 9th Aerospace Sciences