On the fundamental acoustic mode in variable area, low Mach number nozzles
DOI10.1016/0376-0421(85)90003-XzbMath0582.76087OpenAlexW1995549681MaRDI QIDQ3705151
Publication date: 1985
Published in: Progress in Aerospace Sciences (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/0376-0421(85)90003-x
cut-off frequenciesduality principleelementary solutionsequipartition of energyacoustic fieldsExact solutionsacoustic pressureaxially accelerated or decelerated mean flowbiasing of kinetic and compression energiescorrection factor for amplitude and phasefundamental longitudinal modenon-uniform convectionphase lawspropagation of sound in nozzlesquasi-one-dimensional, low Mach number nozzle flowsound in ducts
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