Aeroacoustics of low Mach number flows :: fundamentals, analysis, and measurement /
Focusing both on the necessary mathematics and physics, this resource provides a comprehensive treatment of sound radiation from subsonic flow over moving surfaces, which is the most widespread cause of flow noise in engineering systems. --
Gespeichert in:
Hauptverfasser: | , |
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Format: | Elektronisch E-Book |
Sprache: | English |
Veröffentlicht: |
London :
Academic Press,
[2017]
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Schlagworte: | |
Online-Zugang: | Volltext Volltext |
Zusammenfassung: | Focusing both on the necessary mathematics and physics, this resource provides a comprehensive treatment of sound radiation from subsonic flow over moving surfaces, which is the most widespread cause of flow noise in engineering systems. -- |
Beschreibung: | 1 online resource : illustrations |
Bibliographie: | Includes bibliographical references and index. |
ISBN: | 9780128097939 0128097930 |
Internformat
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100 | 1 | |a Glegg, Stewart A. L., |e author. |0 http://id.loc.gov/authorities/names/no96013765 | |
245 | 1 | 0 | |a Aeroacoustics of low Mach number flows : |b fundamentals, analysis, and measurement / |c Stewart Glegg and William Devenport. |
264 | 1 | |a London : |b Academic Press, |c [2017] | |
264 | 4 | |c ©2017 | |
300 | |a 1 online resource : |b illustrations | ||
336 | |a text |b txt |2 rdacontent | ||
337 | |a computer |b c |2 rdamedia | ||
338 | |a online resource |b cr |2 rdacarrier | ||
347 | |a text file | ||
504 | |a Includes bibliographical references and index. | ||
588 | 0 | |a Online resource; title from PDF title page (EBSCO, viewed March 12, 2017). | |
505 | 0 | |a Front Cover; Aeroacoustics of Low Mach Number Flows: Fundamentals, Analysis, and Measurement; Copyright; Dedication; Contents; Preface; Part 1: Fundamentals; Chapter 1: Introduction; 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; References; Chapter 2: The equations of fluid motion; 2.1. Tensor notation; 2.2. The equation of continuity; 2.3. The momentum equation; 2.3.1. General considerations; 2.3.2. Viscous stresses; 2.4. Thermodynamic quantities. | |
505 | 8 | |a 2.5. The role of vorticity2.5.1. Crocco's equation; 2.5.2. The vorticity equation; 2.5.3. The speed of sound in ideal flow; 2.6. Energy and acoustic intensity; 2.6.1. The energy equation; 2.6.2. Sound power; 2.7. Some relevant fluid dynamic concepts and methods; 2.7.1. Streamlines and vorticity; 2.7.2. Ideal flow; 2.7.3. Conformal mapping; 2.7.4. Vortex filaments and the Biot Savart law; References; Chapter 3: Linear acoustics; 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. | |
505 | 8 | |a 3.5. Sound scattering by a small sphere3.6. 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; References; Chapter 4: Lighthill's acoustic analogy; 4.1. Lighthill's analogy; 4.2. Limitations of the acoustic analogy; 4.2.1. Nearly incompressible flow; 4.2.2. Uniform flow; 4.3. Curle's theorem; 4.4. Monopole, dipole, and quadrupole sources; 4.5. Tailored Green's functions. | |
505 | 8 | |a 4.6. Integral formulas for tailored Green's functions4.7. Wavenumber and Fourier transforms; References; Chapter 5: The Ffowcs Williams and Hawkings equation; 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; References; Chapter 6: The linearized Euler equations; 6.1. Goldstein's equation; 6.2. Drift coordinates; 6.3. Rapid distortion theory; 6.4. Acoustically compact thin airfoils and the Kutta condition. | |
505 | 8 | |a 6.5. The Prantl-Glauert transformationReferences; Chapter 7: Vortex sound; 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; 7.6.1. The effect of angle of attack; 7.6.2. The effect of airfoil thickness; References; Chapter 8: Turbulence and stochastic processes; 8.1. The nature of turbulence; 8.2. Averaging and the expected value. | |
520 | |a Focusing both on the necessary mathematics and physics, this resource provides a comprehensive treatment of sound radiation from subsonic flow over moving surfaces, which is the most widespread cause of flow noise in engineering systems. -- |c Edited summary from book. | ||
650 | 0 | |a Aeroacoustics. |0 http://id.loc.gov/authorities/subjects/sh2011004689 | |
650 | 0 | |a Mach number. |0 http://id.loc.gov/authorities/subjects/sh85079305 | |
650 | 0 | |a Aerodynamic noise. |0 http://id.loc.gov/authorities/subjects/sh85001294 | |
650 | 0 | |a Aerodynamics |x Mathematical models. | |
650 | 6 | |a Aérodynamique |x Modèles mathématiques. | |
650 | 6 | |a Aéroacoustique. | |
650 | 6 | |a Nombre de Mach. | |
650 | 6 | |a Bruit aérodynamique. | |
650 | 7 | |a SCIENCE |x Acoustics & Sound. |2 bisacsh | |
650 | 7 | |a Aerodynamics |x Mathematical models |2 fast | |
650 | 7 | |a Aeroacoustics |2 fast | |
650 | 7 | |a Aerodynamic noise |2 fast | |
650 | 7 | |a Mach number |2 fast | |
655 | 4 | |a Electronic book. | |
700 | 1 | |a Devenport, William J., |e author. |0 http://id.loc.gov/authorities/names/no98054363 | |
758 | |i has work: |a Aeroacoustics of low Mach number flows (Text) |1 https://id.oclc.org/worldcat/entity/E39PCGYwbTDmKfk4pbrJyPFD4q |4 https://id.oclc.org/worldcat/ontology/hasWork | ||
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Datensatz im Suchindex
DE-BY-FWS_katkey | ZDB-4-EBA-ocn973396718 |
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author | Glegg, Stewart A. L. Devenport, William J. |
author_GND | http://id.loc.gov/authorities/names/no96013765 http://id.loc.gov/authorities/names/no98054363 |
author_facet | Glegg, Stewart A. L. Devenport, William J. |
author_role | aut aut |
author_sort | Glegg, Stewart A. L. |
author_variant | s a l g sal salg w j d wj wjd |
building | Verbundindex |
bvnumber | localFWS |
callnumber-first | T - Technology |
callnumber-label | TL574 |
callnumber-raw | TL574.N6 |
callnumber-search | TL574.N6 |
callnumber-sort | TL 3574 N6 |
callnumber-subject | TL - Motor Vehicles and Aeronautics |
collection | ZDB-4-EBA |
contents | Front Cover; Aeroacoustics of Low Mach Number Flows: Fundamentals, Analysis, and Measurement; Copyright; Dedication; Contents; Preface; Part 1: Fundamentals; Chapter 1: Introduction; 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; References; Chapter 2: The equations of fluid motion; 2.1. Tensor notation; 2.2. The equation of continuity; 2.3. The momentum equation; 2.3.1. General considerations; 2.3.2. Viscous stresses; 2.4. Thermodynamic quantities. 2.5. The role of vorticity2.5.1. Crocco's equation; 2.5.2. The vorticity equation; 2.5.3. The speed of sound in ideal flow; 2.6. Energy and acoustic intensity; 2.6.1. The energy equation; 2.6.2. Sound power; 2.7. Some relevant fluid dynamic concepts and methods; 2.7.1. Streamlines and vorticity; 2.7.2. Ideal flow; 2.7.3. Conformal mapping; 2.7.4. Vortex filaments and the Biot Savart law; References; Chapter 3: Linear acoustics; 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 sphere3.6. 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; References; Chapter 4: Lighthill's acoustic analogy; 4.1. Lighthill's analogy; 4.2. Limitations of the acoustic analogy; 4.2.1. Nearly incompressible flow; 4.2.2. Uniform flow; 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 functions4.7. Wavenumber and Fourier transforms; References; Chapter 5: The Ffowcs Williams and Hawkings equation; 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; References; Chapter 6: The linearized Euler equations; 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 transformationReferences; Chapter 7: Vortex sound; 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; 7.6.1. The effect of angle of attack; 7.6.2. The effect of airfoil thickness; References; Chapter 8: Turbulence and stochastic processes; 8.1. The nature of turbulence; 8.2. Averaging and the expected value. |
ctrlnum | (OCoLC)973396718 |
dewey-full | 534/.2 |
dewey-hundreds | 500 - Natural sciences and mathematics |
dewey-ones | 534 - Sound and related vibrations |
dewey-raw | 534/.2 |
dewey-search | 534/.2 |
dewey-sort | 3534 12 |
dewey-tens | 530 - Physics |
discipline | Physik |
format | Electronic eBook |
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isbn | 9780128097939 0128097930 |
language | English |
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spelling | Glegg, Stewart A. L., author. http://id.loc.gov/authorities/names/no96013765 Aeroacoustics of low Mach number flows : fundamentals, analysis, and measurement / Stewart Glegg and William Devenport. London : Academic Press, [2017] ©2017 1 online resource : illustrations text txt rdacontent computer c rdamedia online resource cr rdacarrier text file Includes bibliographical references and index. Online resource; title from PDF title page (EBSCO, viewed March 12, 2017). Front Cover; Aeroacoustics of Low Mach Number Flows: Fundamentals, Analysis, and Measurement; Copyright; Dedication; Contents; Preface; Part 1: Fundamentals; Chapter 1: Introduction; 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; References; Chapter 2: The equations of fluid motion; 2.1. Tensor notation; 2.2. The equation of continuity; 2.3. The momentum equation; 2.3.1. General considerations; 2.3.2. Viscous stresses; 2.4. Thermodynamic quantities. 2.5. The role of vorticity2.5.1. Crocco's equation; 2.5.2. The vorticity equation; 2.5.3. The speed of sound in ideal flow; 2.6. Energy and acoustic intensity; 2.6.1. The energy equation; 2.6.2. Sound power; 2.7. Some relevant fluid dynamic concepts and methods; 2.7.1. Streamlines and vorticity; 2.7.2. Ideal flow; 2.7.3. Conformal mapping; 2.7.4. Vortex filaments and the Biot Savart law; References; Chapter 3: Linear acoustics; 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 sphere3.6. 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; References; Chapter 4: Lighthill's acoustic analogy; 4.1. Lighthill's analogy; 4.2. Limitations of the acoustic analogy; 4.2.1. Nearly incompressible flow; 4.2.2. Uniform flow; 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 functions4.7. Wavenumber and Fourier transforms; References; Chapter 5: The Ffowcs Williams and Hawkings equation; 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; References; Chapter 6: The linearized Euler equations; 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 transformationReferences; Chapter 7: Vortex sound; 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; 7.6.1. The effect of angle of attack; 7.6.2. The effect of airfoil thickness; References; Chapter 8: Turbulence and stochastic processes; 8.1. The nature of turbulence; 8.2. Averaging and the expected value. Focusing both on the necessary mathematics and physics, this resource provides a comprehensive treatment of sound radiation from subsonic flow over moving surfaces, which is the most widespread cause of flow noise in engineering systems. -- Edited summary from book. Aeroacoustics. http://id.loc.gov/authorities/subjects/sh2011004689 Mach number. http://id.loc.gov/authorities/subjects/sh85079305 Aerodynamic noise. http://id.loc.gov/authorities/subjects/sh85001294 Aerodynamics Mathematical models. Aérodynamique Modèles mathématiques. Aéroacoustique. Nombre de Mach. Bruit aérodynamique. SCIENCE Acoustics & Sound. bisacsh Aerodynamics Mathematical models fast Aeroacoustics fast Aerodynamic noise fast Mach number fast Electronic book. Devenport, William J., author. http://id.loc.gov/authorities/names/no98054363 has work: Aeroacoustics of low Mach number flows (Text) https://id.oclc.org/worldcat/entity/E39PCGYwbTDmKfk4pbrJyPFD4q https://id.oclc.org/worldcat/ontology/hasWork Print version: Glegg, Stewart A.L. Aeroacoustics of low Mach number flows. London : Academic Press, [2017] 0128096519 9780128096512 (OCoLC)959872129 FWS01 ZDB-4-EBA FWS_PDA_EBA https://search.ebscohost.com/login.aspx?direct=true&scope=site&db=nlebk&AN=1161626 Volltext FWS01 ZDB-4-EBA FWS_PDA_EBA https://www.sciencedirect.com/science/book/9780128096512 Volltext |
spellingShingle | Glegg, Stewart A. L. Devenport, William J. Aeroacoustics of low Mach number flows : fundamentals, analysis, and measurement / Front Cover; Aeroacoustics of Low Mach Number Flows: Fundamentals, Analysis, and Measurement; Copyright; Dedication; Contents; Preface; Part 1: Fundamentals; Chapter 1: Introduction; 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; References; Chapter 2: The equations of fluid motion; 2.1. Tensor notation; 2.2. The equation of continuity; 2.3. The momentum equation; 2.3.1. General considerations; 2.3.2. Viscous stresses; 2.4. Thermodynamic quantities. 2.5. The role of vorticity2.5.1. Crocco's equation; 2.5.2. The vorticity equation; 2.5.3. The speed of sound in ideal flow; 2.6. Energy and acoustic intensity; 2.6.1. The energy equation; 2.6.2. Sound power; 2.7. Some relevant fluid dynamic concepts and methods; 2.7.1. Streamlines and vorticity; 2.7.2. Ideal flow; 2.7.3. Conformal mapping; 2.7.4. Vortex filaments and the Biot Savart law; References; Chapter 3: Linear acoustics; 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 sphere3.6. 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; References; Chapter 4: Lighthill's acoustic analogy; 4.1. Lighthill's analogy; 4.2. Limitations of the acoustic analogy; 4.2.1. Nearly incompressible flow; 4.2.2. Uniform flow; 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 functions4.7. Wavenumber and Fourier transforms; References; Chapter 5: The Ffowcs Williams and Hawkings equation; 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; References; Chapter 6: The linearized Euler equations; 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 transformationReferences; Chapter 7: Vortex sound; 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; 7.6.1. The effect of angle of attack; 7.6.2. The effect of airfoil thickness; References; Chapter 8: Turbulence and stochastic processes; 8.1. The nature of turbulence; 8.2. Averaging and the expected value. Aeroacoustics. http://id.loc.gov/authorities/subjects/sh2011004689 Mach number. http://id.loc.gov/authorities/subjects/sh85079305 Aerodynamic noise. http://id.loc.gov/authorities/subjects/sh85001294 Aerodynamics Mathematical models. Aérodynamique Modèles mathématiques. Aéroacoustique. Nombre de Mach. Bruit aérodynamique. SCIENCE Acoustics & Sound. bisacsh Aerodynamics Mathematical models fast Aeroacoustics fast Aerodynamic noise fast Mach number fast |
subject_GND | http://id.loc.gov/authorities/subjects/sh2011004689 http://id.loc.gov/authorities/subjects/sh85079305 http://id.loc.gov/authorities/subjects/sh85001294 |
title | Aeroacoustics of low Mach number flows : fundamentals, analysis, and measurement / |
title_auth | Aeroacoustics of low Mach number flows : fundamentals, analysis, and measurement / |
title_exact_search | Aeroacoustics of low Mach number flows : fundamentals, analysis, and measurement / |
title_full | Aeroacoustics of low Mach number flows : fundamentals, analysis, and measurement / Stewart Glegg and William Devenport. |
title_fullStr | Aeroacoustics of low Mach number flows : fundamentals, analysis, and measurement / Stewart Glegg and William Devenport. |
title_full_unstemmed | Aeroacoustics of low Mach number flows : fundamentals, analysis, and measurement / Stewart Glegg and William Devenport. |
title_short | Aeroacoustics of low Mach number flows : |
title_sort | aeroacoustics of low mach number flows fundamentals analysis and measurement |
title_sub | fundamentals, analysis, and measurement / |
topic | Aeroacoustics. http://id.loc.gov/authorities/subjects/sh2011004689 Mach number. http://id.loc.gov/authorities/subjects/sh85079305 Aerodynamic noise. http://id.loc.gov/authorities/subjects/sh85001294 Aerodynamics Mathematical models. Aérodynamique Modèles mathématiques. Aéroacoustique. Nombre de Mach. Bruit aérodynamique. SCIENCE Acoustics & Sound. bisacsh Aerodynamics Mathematical models fast Aeroacoustics fast Aerodynamic noise fast Mach number fast |
topic_facet | Aeroacoustics. Mach number. Aerodynamic noise. Aerodynamics Mathematical models. Aérodynamique Modèles mathématiques. Aéroacoustique. Nombre de Mach. Bruit aérodynamique. SCIENCE Acoustics & Sound. Aerodynamics Mathematical models Aeroacoustics Aerodynamic noise Mach number Electronic book. |
url | https://search.ebscohost.com/login.aspx?direct=true&scope=site&db=nlebk&AN=1161626 https://www.sciencedirect.com/science/book/9780128096512 |
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