Weakly nonlinear acoustic and shock-wave theory of the noise of advanced high-speed turbopropellers

DOI10.1017/S0022112086002501zbMath0619.76086OpenAlexW2097582583MaRDI QIDQ3757600

M. Salikuddin, Christopher K. W. Tam

Publication date: 1986

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/s0022112086002501

zbMATH Keywords

boundary value problemnoise fieldblade fixed coordinate systemhigh speed turbopropellersNonlinear propagation effects

Mathematics Subject Classification ID

Nonlinear effects in hydrodynamic stability (76E30) Shock waves and blast waves in fluid mechanics (76L05) Hydro- and aero-acoustics (76Q05) Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10)

Related Items (1)

Large eddy simulation of flow around a reverse rotating propeller

Cites Work

• On linear acoustic solutions of high speed helicopter impulsive noise problems
• The importance of quadrupole sources in prediction of transonic tip speed propeller noise

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