Table of Contents
Part 1: Fundamentals
1: Introduction
- Abstract
- 1.1 Aeroacoustics of low Mach number flows
- 1.2 Sound waves and turbulence
- 1.3 Quantifying sound levels and annoyance
- 1.4 Symbol and analysis conventions used in this book
2: The equations of fluid motion
- Abstract
- 2.1 Tensor notation
- 2.2 The equation of continuity
- 2.3 The momentum equation
- 2.4 Thermodynamic quantities
- 2.5 The role of vorticity
- 2.6 Energy and acoustic intensity
- 2.7 Some relevant fluid dynamic concepts and methods
3: Linear acoustics
- Abstract
- 3.1 The acoustic wave equation
- 3.2 Plane waves and spherical waves
- 3.3 Harmonic time dependence
- 3.4 Sound generation by a small sphere
- 3.5 Sound scattering by a small sphere
- 3.6 Superposition and far field approximations
- 3.7 Monopole, dipole, and quadrupole sources
- 3.8 Acoustic intensity and sound power output
- 3.9 Solution to the wave equation using Green‘s functions
- 3.10 Frequency domain solutions and Fourier transforms
4: Lighthill‘s acoustic analogy
- Abstract
- 4.1 Lighthill‘s analogy
- 4.2 Limitations of the acoustic analogy
- 4.3 Curle‘s theorem
- 4.4 Monopole, dipole, and quadrupole sources
- 4.5 Tailored Green‘s functions
- 4.6 Integral formulas for tailored Green‘s functions
- 4.7 Wavenumber and Fourier transforms
5: The Ffowcs Williams and Hawkings equation
- Abstract
- 5.1 Generalized derivatives
- 5.2 The Ffowcs Williams and Hawkings equation
- 5.3 Moving sources
- 5.4 Sources in a free stream
- 5.5 Ffowcs Williams and Hawkings surfaces
- 5.6 Incompressible flow estimates of acoustic source terms
6: The linearized Euler equations
- Abstract
- 6.1 Goldstein‘s equation
- 6.2 Drift coordinates
- 6.3 Rapid distortion theory
- 6.4 Acoustically compact thin airfoils and the Kutta condition
- 6.5 The Prantl–Glauert transformation
7: Vortex sound
- Abstract
- 7.1 Theory of vortex sound
- 7.2 Sound from two line vortices in free space
- 7.3 Surface forces in incompressible flow
- 7.4 Aeolian tones
- 7.5 Blade vortex interactions in incompressible flow
- 7.6 The effect of angle of attack and blade thickness on unsteady loads
8: Turbulence and stochastic processes
- Abstract
- 8.1 The nature of turbulence
- 8.2 Averaging and the expected value
- 8.3 Averaging of the governing equations and computational approaches
- 8.4 Descriptions of turbulence for aeroacoustic analysis
9: Turbulent flows
- Abstract
- 9.1 Homogeneous isotropic turbulence
- 9.2 Inhomogeneous turbulent flows
Part 2: Experimental approaches
10: Aeroacoustic testing and instrumentation
- Abstract
- 10.1 Aeroacoustic wind tunnels
- 10.2 Wind tunnel acoustic corrections
- 10.3 Sound measurement
- 10.4 The measurement of turbulent pressure fluctuations
- 10.5 Velocity measurement
11: Measurement, signal processing, and uncertainty
- Abstract
- 11.1 Limitations of measured data
- 11.2 Uncertainty
- 11.3 Averaging and convergence
- 11.4 Numerically estimating fourier transforms
- 11.5 Measurement as seen from the frequency domain
- 11.6 Calculating time spectra and correlations
- 11.7 Wavenumber spectra and spatial correlations
12: Phased arrays
- Abstract
- 12.1 Basic delay and sum processing
- 12.2 General approach to array processing
- 12.3 Deconvolution methods
- 12.4 Correlated sources and directionality
Part 3: Edge and boundary layer noise
13: The theory of edge scattering
- Abstract
- 13.1 The importance of edge scattering
- 13.2 The Schwartzschild problem and its solution based on the Weiner Hopf method
- 13.3 The effect of uniform flow
- 13.4 The leading edge scattering problem
14: Leading edge noise
- Abstract
- 14.1 The compressible flow blade response function
- 14.2 The acoustic far field
- 14.3 An airfoil in a turbulent stream
- 14.4 Blade vortex interactions in compressible flow
15: Trailing edge and roughness noise
- Abstract
- 15.1 The origin and scaling of trailing edge noise
- 15.2 Amiet‘s trailing edge noise theory
- 15.3 The method of *s, Pope, and Marcolini [8]
- 15.4 Roughness noise
Part 4: Rotating blades and duct acoustics
16: Open rotor noise
- Abstract
- 16.1 Tone and broadband noise
- 16.2 Time domain prediction methods for tone noise
- 16.3 Frequency domain prediction methods for tone noise
- 16.4 Broadband noise from open rotors
- 16.5 Haystacking of broadband noise
- 16.6 Blade vortex interactions
17: Duct acoustics
- Abstract
- 17.1 Introduction
- 17.2 The sound in a cylindrical duct
- 17.3 Duct liners
- 17.4 The Green‘s function for a source in a cylindrical duct
- 17.5 Sound power in ducts
- 17.6 Nonuniform mean flow
- 17.7 The radiation from duct inlets and exits
18: Fan noise
- Abstract
- 18.1 Sources of sound in ducted fans
- 18.2 Duct mode amplitudes
- 18.3 The cascade blade response function
- 18.4 The rectilinear model of a rotor or stator in a cylindrical duct
- 18.5 Wake evolution in swirling flows
- 18.6 Fan tone noise
- 18.7 Broadband fan noise
Appendix A: Nomenclature
A.1 Symbol conventions, symbol modifiers, and Fourier transforms
A.2 Symbols used
Appendix B: Branch cuts
Appendix C: The cascade blade response function
Index
Aeroacoustics of Low Mach Number Flows - 1st Edition (elsevier.com)
TOC - aeroacoustics of low mach number - Stewart Glegg, William Devenport