1963
DOI: 10.2514/3.1848
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Jet Noise

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Cited by 165 publications
(47 citation statements)
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“…Accordingly they proposed the existence of two universal (but empirical) similarity spectrum functions F and G , such that the overall jet noise spectrum is expressed as (19) where F(f /fL) is a spectrum for the large-scale turbulence/instability waves (characteristic of It is interesting to note that the Ribner spectrum matches well with the large-scale turbulence noise spectrum due to Tam for frequencies below the peak frequency, whereas it compares better with Tam's fine-scale turbulence noise spectrum beyond the peak frequency except at very large frequencies. The intersection of Tam's large scale and small scale spectra at high frequencies points to a difficulty from the point of view of sound generation.…”
Section: Spectral Distributionmentioning
confidence: 99%
“…Accordingly they proposed the existence of two universal (but empirical) similarity spectrum functions F and G , such that the overall jet noise spectrum is expressed as (19) where F(f /fL) is a spectrum for the large-scale turbulence/instability waves (characteristic of It is interesting to note that the Ribner spectrum matches well with the large-scale turbulence noise spectrum due to Tam for frequencies below the peak frequency, whereas it compares better with Tam's fine-scale turbulence noise spectrum beyond the peak frequency except at very large frequencies. The intersection of Tam's large scale and small scale spectra at high frequencies points to a difficulty from the point of view of sound generation.…”
Section: Spectral Distributionmentioning
confidence: 99%
“…Lighthill 5 derived an equation for the overall sound power for subsonic jets by using available experimental data and dimen sional analysis as…”
Section: Correlation Of Acoustic Data With Jet Noise Theoriesmentioning
confidence: 99%
“…17 -19. 5 Lighthill 4 showed that a fluctuating flow of gas in a turbu lent jet generates in the surrounding atmospnere the same fluctuations of density as would be produced in a classical stationary acoustic medium by a system of external applied stresses. And the radiated sound is due to the turnulent flow which does not react significantly upon it for subsonic flow velocities.…”
mentioning
confidence: 99%
“…19b. Downstream of the supersonic region in the fully developed subsonic turbulent flow the acoustic radiation per unit length of the jet decreased as x~6, which was postulated by Lighthill 17 for a subsonic jet. where m = PJ UjA is the mass flow of the jet.…”
Section: Axial Piezoelectric Impact Pressure Fluctuationsmentioning
confidence: 95%