Aeroacoustics of Low Mach Number Flows: Fundamentals, Analysis, and Measurement
Autor Stewart Glegg, William Devenporten Limba Engleză Paperback – 14 feb 2017
Beginning with fluid dynamics, the fundamental equations of aeroacoustics are derived and the key methods of solution are explained, focusing both on the necessary mathematics and physics. Fundamentals of turbulence and turbulent flows, experimental methods and numerous applications are also covered.
The book is an ideal source of information on aeroacoustics for researchers and graduate students in engineering, physics, or applied math, as well as for engineers working in this field.
Supplementary material for this book is provided by the authors on the website www.aeroacoustics.net. The website provides educational content designed to help students and researchers in understanding some of the principles and applications of aeroacoustics, and includes example problems, data, sample codes, course plans and errata. The website is continuously being reviewed and added to.
- Explains the key theoretical tools of aeroacoustics, from Lighthill’s analogy to the Ffowcs Williams and Hawkings equation
- Provides detailed coverage of sound from lifting surfaces, boundary layers, rotating blades, ducted fans and more
- Presents the fundamentals of sound measurement and aeroacoustic wind tunnel testing
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Specificații
ISBN-13: 9780128096512
ISBN-10: 0128096519
Pagini: 552
Dimensiuni: 152 x 229 x 32 mm
Greutate: 0.73 kg
Editura: ELSEVIER SCIENCE
ISBN-10: 0128096519
Pagini: 552
Dimensiuni: 152 x 229 x 32 mm
Greutate: 0.73 kg
Editura: ELSEVIER SCIENCE
Public țintă
Researchers and grad students in engineering, physics or applied math with an interest in hydro or aeroacoustics. Also engineers working in aeroacoustics and fluid dynamicsCuprins
Part 1: Fundamentals1. Introduction2. The equations of fluid motion3. Linear acoustics4. Lighthill's acoustic analogy5. The Ffowcs Williams and Hawkings equation6. The linearized Euler equations7. Vortex sound8. Turbulence and stochastic processes9. Turbulent flows
Part 2: Experimental approaches10. Aeroacoustic testing and instrumentation11. Measurement, signal processing, and uncertainty12. Phased arrays
Part 3: Edge and boundary layer noise13. The theory of edge scattering14. Leading edge noise15. Trailing edge and roughness noise
Part 4: Rotating blades and duct acoustics16. Open rotor noise17. Duct acoustics18. Fan noise
Part 2: Experimental approaches10. Aeroacoustic testing and instrumentation11. Measurement, signal processing, and uncertainty12. Phased arrays
Part 3: Edge and boundary layer noise13. The theory of edge scattering14. Leading edge noise15. Trailing edge and roughness noise
Part 4: Rotating blades and duct acoustics16. Open rotor noise17. Duct acoustics18. Fan noise
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