“…The Harper-Bourne 11,12 and NASA experiments 2,8,9 have both found similar generic behavior as Tanna 1 and Tanna et al 14 measurements quantify the reduction in core length with an appropriate reduction in turbulence convection velocity (see Bridges & Wernet 2 also), which might indicate the weakness of the sound source in heated supersonic flows. Although the Ma and T R of these studies are somewhat beyond our concerns (involving supersonic source convection effects), Liu et al ( 17 , p.6) indicate that sound radiated by Mach waves is expected to enter at high frequencies at these speeds, hence the Shea/Stuber results 15,16 will be qualitatively applicable to the mild supersonic conditions under our consideration in which sound amplification due to turbulence/mean flow interaction (i.e. jet quietening effects) remain a low frequency phenomenon.…”