1. 1Viswanathan,K.ʺAeroacousticsofHotJets,ʺJournalofFluidMechanics,Vol.516.Oct.2004. Figure 31. Jet noise from nozzle with extensions to increase the boundary layer for a jet with a pressure ratio of 1.229. (a) Polar angle of 30°, (b) Polar angle of 90°. Reproduced fromAhuja13.
2. 2Viswanathan,K.andCzech,M.J.ʺ oleofJetTemperatureinCorrelatingJetNoise,ʺ AIAAJournal,Vol.47,No.5.May2009.
3. 3Tanna, H. K., Dean, P. D., and Burrin, H. ʺThe Generation and adiation of Supersonic Jet Noise. Volume 3: Turbulent MixingNoiseData[Final Technical Report,6 Nov.1972 -6 Nov.1975],ʺ1976.