Abstract
Nomenclature A parameter given by Eq. (6a) B = parameter given by Eq. (6b) C = parameter given by Eq. (6c) CD = drag coefficient CF = thrust coefficient D = plume drag F = missile thrust h = enthalpy M = Mach number P = static pressure q = dynamic pressure R = gas constant r = plume radius AS = entropy change T = plume temperature v = plume velocity 7 = ratio of specific heats e = expansion ratio p = plume density £ = parameter given by Eq. (5) or (9)
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