THESE de DOCTORAT - cerfacs
THESE de DOCTORAT - cerfacs THESE de DOCTORAT - cerfacs
130 BIBLIOGRAPHY [30] FRAYSSÉ, V., GIRAUD, L., AND GRATTON, S. A set of flexible GMRES routines for real and complex arithmetics on high performance computers. Tech. rep., CERFACS, 2007. [31] GOLDSTEIN, M. E. Aeroacoustics. McGraw-Hill, New York, 1976. [32] HASSAN, H. Scaling of combustion generated noise. J. Fluid Mech. 49 (1974), 445–453. [33] HELLEY, P. L. Etude théorique et expérimentale des intabilités de combustion et de leur contrôle dans un bruleur laminaire prémélangé. PhD thesis, Ecole Centrale Paris, 1994. [34] HURLE, I. R., PRICE, R. B., SUDGEN, T. M., AND THOMAS, A. Sound emission from open turbulent premixed flames. Proc. R. Soc. Lond. 303 (1968), 409–427. [35] ICAO. Growth air traffic projected to continue to 2025: www.icao.int/icao/en/nr/2007/pio200708_e.pdf, 2007. [36] IHME, M., PITSCH, H., AND BODONY, H. Radiation of noise in turbulent flames. Proc. Combust. Inst. 32 (2009), 1545–1554. [37] KAUFMANN, A., NICOUD, F., AND POINSOT, T. Flow forcing techniques for numerical simulation of combustion instabilities. Combust. Flame 131 (2002), 371–385. [38] KLEIN, S. A. On the acoustics of turbulent non-premixed flames. PhD thesis, Universit de Twente, 2000. [39] KOTAKE, S. On combustion noise related to chemical reactions. J. Sound Vib. 42 (1975), 399–410. [40] KOTAKE, S., AND HATTA, K. On the noise of diffusion flames. Japan Society of Mechanical Engineers Journal (1965), 211–219. [41] LAMARQUE, N., AND POINSOT, T. Boundary conditions fo acoustic eigenmode computations in gas turbine combustion chambers. AIAA Journal 46, 9 (2008), 2282–2292. [42] LAMARQUE, N., PORTA, M., NICOUD, F., AND POINSOT, T. On the stability and dissipation of wall boundary conditions for compressible flows. Int. J. Numer. Meth. Fluids 62 (2010), 1134–1154. [43] LAMRAOUI, A., AND ET AL. Acoustic reconstruction of the fuel and air feeding line impedances in a swirled burner during combustion instabilities. In 3rd European Conference for Aerospace Sciences EUCASS (2009). [44] LAMRAOUI, A., RICHECOEUR, F., SCHULLER, T., AND DUCRUIX, S. Methodology for on the fly acoustic characterization of the feedings lines impedances in a turbulent swirled combustor. In Proceedings of ASME Turbo Expo 2010: Power for Land, Sea and Air (2010). [45] LAWSON, C. L., AND HANSON, R. J. Solving Least Squares Problems. SIAM Classics in Applied Mechanics, 1974. [46] LEROYER, P. Airside study of Charles de Gaulle airport. Tech. rep., Airside Organization. Traffic Growth and Risks of Congestion. MIT, 2004.
BIBLIOGRAPHY 131 [47] LEYKO, M., NICOUD, F., AND POINSOT, T. Comparison of direct and indirect combustion noise mechanisms in a model combustor. AIAA Journal 47, 11 (2009), 2709–2716. [48] LIEUWEN, T., AND YANG, V. Combustion instabilities in gas turbine engines. operational experience, fundamental mechanisms and modeling. In Prog. in Astronautics and Aeronautics AIAA (2005), vol. 210. [49] LIEUWEN, T., AND ZINN, B. T. The role of equivalence ratio oscillations in driving combustion instabilities in low NOx gas turbines. Proc. Combust. Inst. 27 (1998), 1809– 1816. [50] LIGHTHILL, M. J. On sound generated aerodynamically: I. general theory. Proc. R. Soc. Lond. 211, 1107 (1952), 564–587. [51] LIGHTHILL, M. J. On sound generated aerodynamically: II. turbulence as a source of sound. Proc. R. Soc. Lond. 222 (1954), 1–32. [52] LILLEY, G. M. The generation and radiation of supersonic jet noise vol iv - Theory of turbulence generated jet noise, noise radiation from upstream sources, and combustion noise. part II: Generation of sound in a mixing regionheory of turbulence generated jet noise, noise radiation from upstream sources, and combustion noise. part II: Generation of sound in a mixing region. Afapl-tr-72-53, Air Force Aero Propulsion Laboratory, 1972. [53] LILLEY, G. M. On the noise from jets. Agard cp-131, 1974. [54] LYRINTZIS, A. S. Integral acoustic methods: From the (cfd) near-field to the (acoustic) far-field. International Journal of Aeroacoustics 2 (2003), 95–128. [55] MARBLE, F. E., AND CANDEL, S. Acoustic disturbances from gas nonuniformities convected through a nozzle. J. Sound Vib. 55 (1977), 225–243. [56] MARTIN, C., BENOIT, L., SOMMERER, Y., NICOUD, F., AND POINSOT, T. LES and acoustic analysis of combustion instability in a staged turbulent swirled combustor. AIAA Journal 44, 4 (2006), 741–750. [57] MENDEZ, S., AND NICOUD, F. Large eddy simulation of a bi-periodic turbulent flow with effusion. J. Fluid Mech. 598 (2008), 27–65. [58] MILLER, N. P., REINDEL, E. M., AND HORONJEFF, R. D. Aircraft and airport noise prediction and control. Handbook of Noise and Vibration Control. Malcolm J. Crocker, 2007. [59] MOASE, W., BREAR, M., AND MANZIE, C. The forced response of chocked nozzles and supersonic diffusers. J. Fluid Mech. (2007). [60] MOREAU, S., AND ROGER, M. Effect of airfoil aerodynamic loading on trailing-edge noise sources. AIAA Journal 43, 1 (2005), 41–52. [61] MORFEY, C. L. Amplification of aerodynamic noise by convected flow inhomogeneities. J. Sound Vib. 31 (1973), 391–397.
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BIBLIOGRAPHY 131<br />
[47] LEYKO, M., NICOUD, F., AND POINSOT, T. Comparison of direct and indirect combustion<br />
noise mechanisms in a mo<strong>de</strong>l combustor. AIAA Journal 47, 11 (2009), 2709–2716.<br />
[48] LIEUWEN, T., AND YANG, V. Combustion instabilities in gas turbine engines. operational<br />
experience, fundamental mechanisms and mo<strong>de</strong>ling. In Prog. in Astronautics<br />
and Aeronautics AIAA (2005), vol. 210.<br />
[49] LIEUWEN, T., AND ZINN, B. T. The role of equivalence ratio oscillations in driving<br />
combustion instabilities in low NOx gas turbines. Proc. Combust. Inst. 27 (1998), 1809–<br />
1816.<br />
[50] LIGHTHILL, M. J. On sound generated aerodynamically: I. general theory. Proc. R. Soc.<br />
Lond. 211, 1107 (1952), 564–587.<br />
[51] LIGHTHILL, M. J. On sound generated aerodynamically: II. turbulence as a source of<br />
sound. Proc. R. Soc. Lond. 222 (1954), 1–32.<br />
[52] LILLEY, G. M. The generation and radiation of supersonic jet noise vol iv - Theory of<br />
turbulence generated jet noise, noise radiation from upstream sources, and combustion<br />
noise. part II: Generation of sound in a mixing regionheory of turbulence generated<br />
jet noise, noise radiation from upstream sources, and combustion noise. part II:<br />
Generation of sound in a mixing region. Afapl-tr-72-53, Air Force Aero Propulsion Laboratory,<br />
1972.<br />
[53] LILLEY, G. M. On the noise from jets. Agard cp-131, 1974.<br />
[54] LYRINTZIS, A. S. Integral acoustic methods: From the (cfd) near-field to the (acoustic)<br />
far-field. International Journal of Aeroacoustics 2 (2003), 95–128.<br />
[55] MARBLE, F. E., AND CANDEL, S. Acoustic disturbances from gas nonuniformities convected<br />
through a nozzle. J. Sound Vib. 55 (1977), 225–243.<br />
[56] MARTIN, C., BENOIT, L., SOMMERER, Y., NICOUD, F., AND POINSOT, T. LES and acoustic<br />
analysis of combustion instability in a staged turbulent swirled combustor. AIAA<br />
Journal 44, 4 (2006), 741–750.<br />
[57] MENDEZ, S., AND NICOUD, F. Large eddy simulation of a bi-periodic turbulent flow<br />
with effusion. J. Fluid Mech. 598 (2008), 27–65.<br />
[58] MILLER, N. P., REINDEL, E. M., AND HORONJEFF, R. D. Aircraft and airport noise<br />
prediction and control. Handbook of Noise and Vibration Control. Malcolm J. Crocker,<br />
2007.<br />
[59] MOASE, W., BREAR, M., AND MANZIE, C. The forced response of chocked nozzles and<br />
supersonic diffusers. J. Fluid Mech. (2007).<br />
[60] MOREAU, S., AND ROGER, M. Effect of airfoil aerodynamic loading on trailing-edge<br />
noise sources. AIAA Journal 43, 1 (2005), 41–52.<br />
[61] MORFEY, C. L. Amplification of aerodynamic noise by convected flow inhomogeneities.<br />
J. Sound Vib. 31 (1973), 391–397.
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