Shocks and singularities in the pressure field of a supersonically rotating propeller

DOI10.1017/S0022112088001752zbMath0644.76071OpenAlexW1970950530MaRDI QIDQ3787690

C. J. Chapman

Publication date: 1988

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

Full work available at URL: https://doi.org/10.1017/s0022112088001752

zbMATH Keywords

linear acoustic theorysupersonic propellerthickness noise problem

Mathematics Subject Classification ID

Transonic flows (76H05) Hydro- and aero-acoustics (76Q05) Supersonic flows (76J20) Basic methods in fluid mechanics (76M99)

Related Items

Large eddy simulation of flow around a reverse rotating propeller ⋮ Lighthill quadrupole radiation in supersonic propeller acoustics ⋮ Time-domain analysis of contra-rotating propeller noise: wake interaction with a downstream propeller blade ⋮ The breakdown of the linearized theory and the role of quadrupole sources in transonic rotor acoustics

Cites Work

• On the propagation of weak shock waves
• On linear acoustic solutions of high speed helicopter impulsive noise problems
• On the propagation of weak and moderately strong, curved shock waves
• Focusing of weak shock waves at an arête