Aeroacoustics of Low Mach Number Flows: Fundamentals, Analysis and Measurement
Autor Stewart Glegg, William Devenporten Limba Engleză Paperback – 27 sep 2023
New support materials for this edition include course outlines, problem sets, sample MATLAB codes and experimental data to be found at www.aeroacoustics.net.
- Addresses, in detail, sound from rotating blades, ducted fans, airframes, boundary layers, and more
- Presents theory in such a way that it can be used in computational methods and calculating sound levels
- Includes coverage of different experimental approaches to this subject
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Specificații
ISBN-13: 9780443191121
ISBN-10: 0443191123
Pagini: 722
Dimensiuni: 152 x 229 mm
Ediția:2
Editura: ELSEVIER SCIENCE
ISBN-10: 0443191123
Pagini: 722
Dimensiuni: 152 x 229 mm
Ediția:2
Editura: ELSEVIER SCIENCE
Public țintă
Graduate students and researchers with an interest in hydroacoustics or aeroacousticsCuprins
Part 1: Fundamentals
1. Introduction
2. The equations of fluid motion
3. Linear acoustics
Part 2: Fundamentals of Aeroacoustics
4. Lighthill's acoustic analogy
5. The Ffowcs Williams and Hawkings Equation
6. Propeller and Open Rotor Noise
Part 3: Unsteady Blade Loading
7. Amiet’s approach – the Surface Source for Thin Airfoils
8. Goldstein’s approach – flows with distortion
9. Howe’s and Powell’s approach - vortex sound
Part 4: Turbulent Flows
10. Stochastic processes
11. Turbulence and Turbulent Flows
12. Wall Pressure Fluctuations in Turbulent Boundary Layers
Part 5: Broadband Flow Noise from Surface Interactions and Fans
13. Broadband Noise from Open Rotors and Leading-edge Noise
14. Trailing Edge and Roughness Noise
15. Duct Acoustics
16. Fan Noise
Part 6: Experimental Methods
17. Aeroacoustic Testing and Instrumentation
18. Measurement, Signal Processing and Uncertainty
19. Phased Arrays
Part 7 Advanced Mathematical Methods
20. The Theory of Edge Scattering
1. Introduction
2. The equations of fluid motion
3. Linear acoustics
Part 2: Fundamentals of Aeroacoustics
4. Lighthill's acoustic analogy
5. The Ffowcs Williams and Hawkings Equation
6. Propeller and Open Rotor Noise
Part 3: Unsteady Blade Loading
7. Amiet’s approach – the Surface Source for Thin Airfoils
8. Goldstein’s approach – flows with distortion
9. Howe’s and Powell’s approach - vortex sound
Part 4: Turbulent Flows
10. Stochastic processes
11. Turbulence and Turbulent Flows
12. Wall Pressure Fluctuations in Turbulent Boundary Layers
Part 5: Broadband Flow Noise from Surface Interactions and Fans
13. Broadband Noise from Open Rotors and Leading-edge Noise
14. Trailing Edge and Roughness Noise
15. Duct Acoustics
16. Fan Noise
Part 6: Experimental Methods
17. Aeroacoustic Testing and Instrumentation
18. Measurement, Signal Processing and Uncertainty
19. Phased Arrays
Part 7 Advanced Mathematical Methods
20. The Theory of Edge Scattering
Recenzii
"In summary, this is an excellent new reference book for scientists and engineers with interests in the fields of aerodynamics and acoustics. The book is a comprehensive and authoritative new treatise on aeroacoustics and highly recommended for readers familiar with or new to this field." --The Aeronautical Journal
"Aeroacoustics of Low Mach Number Flows is a timely and impressive new book describing the formative developments in aeroacoustics, as well as more recent progress in the field. ...In summary, this is an excellent new reference book for scientists and engineers with interests in the fields of aerodynamics and acoustics. The book is a comprehensive and authoritative new treatise on aeroacoustics and highly recommended for readers familiar with or new to this field." -The Aeronautical Journal
"Aeroacoustics of Low Mach Number Flows is a timely and impressive new book describing the formative developments in aeroacoustics, as well as more recent progress in the field. ...In summary, this is an excellent new reference book for scientists and engineers with interests in the fields of aerodynamics and acoustics. The book is a comprehensive and authoritative new treatise on aeroacoustics and highly recommended for readers familiar with or new to this field." -The Aeronautical Journal