Bibliografías temáticas / Aerodynamic and acoustic data

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Literatura académica sobre el tema "Aerodynamic and acoustic data"

Autor: Grafiati
Publicado: 4 de junio de 2021
Última modificación: 1 de febrero de 2022

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Artículos de revistas sobre el tema "Aerodynamic and acoustic data"

1

Mahdal, Miroslav, Josef Dobeš, and Milada Kozubková. "Measurement of Aerodynamic and Acoustic Quantities Describing Flow around a Body Placed in a Wind Tunnel." Measurement Science Review 19, no. 1 (2019): 20–28. http://dx.doi.org/10.2478/msr-2019-0004.

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Abstract Aerodynamically generated noise affects passenger comfort in cars, high-speed trains, and airplanes, and thus, automobile manufacturers aim for its reduction. Investigation methods of noise and vibration sources can be divided into two groups, i.e. experimental research and mathematical research. Recently, owing to the increase in computing power, research in aerodynamically generated noise (aero-acoustics) is beginning to use modern methods such as computational fluid dynamics or fluid-structure interaction. The mathematical model of turbulent flow is given by the system of partial d
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Patel, Rita R., Shaheen N. Awan, Julie Barkmeier-Kraemer, et al. "Recommended Protocols for Instrumental Assessment of Voice: American Speech-Language-Hearing Association Expert Panel to Develop a Protocol for Instrumental Assessment of Vocal Function." American Journal of Speech-Language Pathology 27, no. 3 (2018): 887–905. http://dx.doi.org/10.1044/2018_ajslp-17-0009.

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Purpose The aim of this study was to recommend protocols for instrumental assessment of voice production in the areas of laryngeal endoscopic imaging, acoustic analyses, and aerodynamic procedures, which will (a) improve the evidence for voice assessment measures, (b) enable valid comparisons of assessment results within and across clients and facilities, and (c) facilitate the evaluation of treatment efficacy. Method Existing evidence was combined with expert consensus in areas with a lack of evidence. In addition, a survey of clinicians and a peer review of an initial version of the protocol
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3

Guérin, S., R. Schnell, and R. G. Becker. "Performance prediction and progress towards multi-disciplinary design of contra-rotating open rotors." Aeronautical Journal 118, no. 1208 (2014): 1159–79. http://dx.doi.org/10.1017/s0001924000009830.

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Abstract At DLR’s Institute of Propulsion Technology, the prediction tools and multi-disciplinary optimisation strategies developed for turbofan engines have been extended to contra-rotating open rotors (CROR). Thereby the objective has been to appraise and improve the performance of CROR engines and thus to reduce their environmental impact. The present paper reviews the intermediate progress achieved in this scope. The prediction is based on analytical and CFD methods and covers the fields of engine performance analysis, aerodynamics and acoustics. The aerodynamic and acoustic results could
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4

Zheng, Zhengyu. "Prediction of dipole sources and aeroacoustics field for tandem cylinder flow field based on DBEM/hybrid LES." International Journal of Aeroacoustics 20, no. 1-2 (2021): 157–73. http://dx.doi.org/10.1177/1475472x20984092.

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In this paper, the DBEM/Hybrid LES（Directly Boundary Element Method/Hybrid Large Eddy Simulation）technique is applied to predict the aerodynamic noise generated by tandem circular cylinders immersed in a three-dimensional turbulent flow. Utilizing the Lighthill's Acoustic Analogy, the flow pressure fluctuation near the surface of the cylinder is converted into acoustic dipole sources. Taking the dipole sound sources as the actual sound sources, the aeroacoustic field is simulated and analyzed by DBEM. The research shows that: The strong dipole sources are distributed in the collision zone of t
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5

Buffum, D. H., and S. Fleeter. "Effect of Wind Tunnel Acoustic Modes on Linear Oscillating Cascade Aerodynamics." Journal of Turbomachinery 116, no. 3 (1994): 513–24. http://dx.doi.org/10.1115/1.2929440.

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The aerodynamics of a biconvex airfoil cascade oscillating in torsion is investigated using the unsteady aerodynamic influence coefficient technique. For subsonic flow and reduced frequencies as large as 0.9, airfoil surface unsteady pressures resulting from oscillation of one of the airfoils are measured using flush-mounted high-frequency-response pressure transducers. The influence coefficient data are examined in detail and then used to predict the unsteady aerodynamics of a cascade oscillating at various interblade phase angles. These results are correlated with experimental data obtained
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6

Andreassen, Meri L., Herbert A. Leeper, Duncan L. Macrae, and Ian R. Nicholson. "Aerodynamic, Acoustic, and Perceptual Changes following Adenoidectomy." Cleft Palate-Craniofacial Journal 31, no. 4 (1994): 263–70. http://dx.doi.org/10.1597/1545-1569_1994_031_0263_aaapcf_2.3.co_2.

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Fourteen children were seen prior to adenoidectomy and at 1 month, 3 months, and 6 months following surgery. On each visit, nasal airway resistance values, nasal cross-sectional area estimates, nasalance scores, and perceptual ratings of nasality were collected. These data were analyzed to identify changes that were related to the time of the test, and to the primary indication for surgery (nasal airway obstruction or recurrent infection). Results revealed significant reduction in nasal airway resistance and significant changes in nasalance following surgery. Perceptual changes were not signif
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7

Cican, Grigore, and Daniel Eugeniu Crunteanu. "Aerodynamic Noise Control Study of Nozzles with Triangular Chevrons." Applied Mechanics and Materials 436 (October 2013): 25–31. http://dx.doi.org/10.4028/www.scientific.net/amm.436.25.

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This paper has a small part of notion of chevron and the process that helps reducing the noise pollution. Based on the gas dynamic and geometrical parameters of a single flow jet engine one does a model of CFD data processing. In this process one observes the influence of chevrons on acoustic wave intensity produced by the jet . One studies a series of tests on triangular chevrons: immersions, the influence of the number of chevrons in order to settle the influence of the geometrical parameters on the flow and on the jet acoustics. Finally one presents the contribution of chevrons in noise pol
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Fan, Feng, Yaxiong Cao, Lusheng Jiang, and Yongfeng Lin. "Research on Calculation Method for Acoustic Scattering of Helicopter Noise." Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 38, no. 6 (2020): 1275–83. http://dx.doi.org/10.1051/jnwpu/20203861275.

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A new calculation method of helicopter rotor/fuselage acoustic scattering is developed. Firstly, a CFD analysis model is developed to simulate flow field of the rotor, which is based on the motional embedded grid system and RANS equations, and provides aerodynamic data for rotor noise calculation. Then, FW-H equations are employed to calculate the aeroacoustic characteristics of isolated rotor, and G 1A formulas are applied to calculate the rotor acoustic gradient to provide boundary condition for acoustic scattering. Based on these, the time-domain equivalent source method is applied to calcu
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9

MacEachern, Margaret R. "Computer modeling of the production of ejectives using aerodynamic and acoustic data." Journal of the Acoustical Society of America 100, no. 4 (1996): 2661. http://dx.doi.org/10.1121/1.417461.

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Shendge, Smit. "Study and Design Frontal Area of a Car to Curtail Aerodynamic Noise." International Journal for Research in Applied Science and Engineering Technology 9, no. 8 (2021): 1637–52. http://dx.doi.org/10.22214/ijraset.2021.37640.

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Abstract: In this field of comparative research study, comparison of two car model, a standard car and an optimized car with respect to aerodynamic analysis/aeroacoustics analysis with the help of CFD software Ansys 2019 R2 version is taken in consideration to compare the results and get to know if the optimized car model has reduction in the generation of aerodynamic noise when it travels at four different speeds (30 m/s, 40 m/s, 50m/s and 60m/s). For carried out aeroacoustics/aerodynamic noise analysis two main model are used turbulence model and an acoustics model. For turbulence model and
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Tesis sobre el tema "Aerodynamic and acoustic data"

1

White, Peta. "Acoustic and aerodynamic measurements of children's voices." Thesis, University of Surrey, 1997. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.388787.

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Xiu, Noé. "Perturbation de la production de la parole chez le patient atteint d'une paralysie laryngée : données acoustiques et aérodynamiques." Thesis, Strasbourg, 2018. http://www.theses.fr/2018STRAC039/document.

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Notre thèse vise à étudier les conséquences d’une ablation totale ou partielle de la glande thyroïde suite à un dysfonctionnement thyroïdien, suivie ou non d’un traitement radiothérapique, et ce dans le domaine de la phonétique clinique. Ce type d’intervention perturbe généralement le système de production de la parole et conduit parfois à une dégradation de la qualité vocale de façon permanente (moins de 5% des cas) ou passagère. Le travail se veut une contribution aux recherches menées en linguistique et phonétique cliniques, plus particulièrement dans le cadre de l’analyse de faits compensa
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Gonçalves, Da Silva Pinto Wagner José. "Modelling airframe noise : from aerodynamic topology to acoustic efficiency." Thesis, Poitiers, 2019. http://www.theses.fr/2019POIT2289.

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L’influence de la forme de cylindres longs sur leur rayonnement acoustique en écoulement est étudiée. Des simulations bidimensionnelles (2D) sont réalisées à bas nombre de Reynolds (Re=20-200), à l’aide du code de calcul direct (DNS) incompressible incompact3D au moyen d’une méthode de frontière immergée (IBM). Une formule dérivée de l’équation de Curle pour un cylindre compact permet la quantification de l’émission acoustique en 2D. En soufflerie anéchoïque, la signature acoustique d’une trentaine de géométries est mesurée, Re=4,000-53,000 ; l’anémométrie par fil chaud est utilisée pour la de
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Goupil, Marc Y. "Dynamic Pressure Sensing for the Flight Test Data System." DigitalCommons@CalPoly, 2019. https://digitalcommons.calpoly.edu/theses/2115.

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This thesis describes the design, assembly, and test of the FTDS-K, a new device in the Boundary Layer Data System (BLDS) family of flight data acquisition systems. The FTDS-K provides high-frequency, high-gain data acquisition capability for up to two pressure sensors and an additional three low-frequency pressure sensors. Development of the FTDS-K was separated into a core module, specialized analog subsystem, and practical testing of the FTDS-K in a flow measurement mission. The core module combines an nRF52840-based microcontroller module, switching regulator, microSD card, real-time clock
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5

Andreou, Christodoulos. "Acoustic and aerodynamic properties of aerofoil leading-edge high-lift geometries." Thesis, University of Cambridge, 2009. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.611404.

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Kutluay, Umit. "Aerodynamic Parameter Estimation Using Flight Test Data." Phd thesis, METU, 2011. http://etd.lib.metu.edu.tr/upload/12613786/index.pdf.

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This doctoral study aims to develop a methodology for use in determining aerodynamic models and parameters from actual flight test data for different types of autonomous flight vehicles. The stepwise regression method and equation error method are utilized for the aerodynamic model identification and parameter estimation. A closed loop aerodynamic parameter estimation approach is also applied in this study which can be used to fine tune the model parameters. Genetic algorithm is used as the optimization kernel for this purpose. In the optimization scheme, an input error cost function is used
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Bilgic, Kemal Onder. "Aerial Acoustic Data Communication." Master's thesis, METU, 2012. http://etd.lib.metu.edu.tr/upload/12614651/index.pdf.

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Spectrum has been a scarce commodity in RF communication. Acoustic data communication is an alternative to RF communication where data is transmitted through sound waves. In this thesis, several different aspects of acoustic data communication are investigated. A physical test setup is built where the data communication spectrum extends up to 40 kHz. Impulse response of the acoustic channel is considered in a laboratory environment. Acoustic spectrum beyond the hearing limit between 25 kHz to 35 kHz is found as a suitable band for the developed setup. Distance and multipath components are impo
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8

Kim, Y. S. "An acoustic, aerodynamic and perceptual investigation of word-initial denasalization in Korean." Thesis, University College London (University of London), 2011. http://discovery.ucl.ac.uk/1324541/.

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Korean nasals /m/ and /n/ are generally considered by Korean phoneticians to be hardly different from the corresponding English sounds, but those in word-initial position are often perceived as plosives by native speakers of English. This had been noted by only a few previous observers, and investigated on a very limited scale. In this study, various experimental methods were employed in systematic analyses of the production and acoustic form of word-initial /m/ and /n/ from fluent connected speech collected from a relatively large number of informants, and corresponding perception tests were
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Albisser, Marie. "Identification of aerodynamic coefficients from free flight data." Thesis, Université de Lorraine, 2015. http://www.theses.fr/2015LORR0083/document.

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L'utilisation des coefficients aérodynamiques pour caractériser le comportement d'un objet en vol libre demeure un sujet de recherche parmi les plus complexes et les plus étudiés dans le domaine de la balistique extérieure. La présente étude analyse l'identification des coefficients aérodynamiques à partir de données obtenues lors d'essais en vol libre. Elle vise à modéliser, définir ainsi que maîtriser les techniques d'identification de paramètres les plus adaptées au problème qu'est la détermination des coefficients aérodynamiques. Le travail de thèse a été dédié au développement d'une procé
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Nelson, Wendy Jill. "Acoustic, physiologic, and aerodynamic effects of the clinical stimulation technique "tongue protrusion/i/" /." abstract and full text PDF (UNR users only), 1998. http://0-gateway.proquest.com.innopac.library.unr.edu/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqdiss&rft_dat=xri:pqdiss:1389835.

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Libros sobre el tema "Aerodynamic and acoustic data"

1

Cross, Jeffrey L. Tip aerodynamics and acoustics test: A report and data survey. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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White, Petra. Acoustic and aerodynamic measurements of children's voices. [University of Surrey], 1997.

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3

Chan, Y. T. Underwater Acoustic Data Processing. Springer Netherlands, 1989.

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NATO Advanced Study Institute on Underwater Acoustic Data Processing (1988 Kingston, Ont.). Underwater acoustic data processing. Kluwer Academic Publishers, 1989.

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Chan, Y. T., ed. Underwater Acoustic Data Processing. Springer Netherlands, 1989. http://dx.doi.org/10.1007/978-94-009-2289-1.

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Weiland, Claus. Aerodynamic data of space vehicles. Springer, 2014.

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Weiland, Claus. Aerodynamic Data of Space Vehicles. Springer Berlin Heidelberg, 2014. http://dx.doi.org/10.1007/978-3-642-54168-1.

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Unit, Engineering Sciences Data. Engineering sciences data: Acoustic fatigue. Engineering Sciences Data Unit, 1991.

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Soderman, Paul T. Acoustic and aerodynamic study of a pusher-propeller aircraft model. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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Wieseman, Carol D. Methodology for matching experimental and computational aerodynamic data. National Aeronautics and Space Administration, Langley Research Center, 1988.

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Capítulos de libros sobre el tema "Aerodynamic and acoustic data"

1

Kim, Hyunsoon, Shinji Maeda, Kiyoshi Honda, and Stephane Hans. "The laryngeal characterization of Korean fricatives: Acoustic and aerodynamic data." In Turbulent Sounds. DE GRUYTER MOUTON, 2010. http://dx.doi.org/10.1515/9783110226584.143.

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Dejonckere, P. H., and G. Wieneke. "9. Cepstra of normal and pathological voices in correlation to acoustical, aerodynamic and perceptual data." In Studies in Speech Pathology and Clinical Linguistics. John Benjamins Publishing Company, 1996. http://dx.doi.org/10.1075/sspcl.6.13dej.

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Aubrun, Sandrine, Alain Seraudie, Daniel Biron, and Daniel Arnal. "Influence of Acoustic Excitation on 3D Boundary Layer Instabilities." In Aerodynamic Drag Reduction Technologies. Springer Berlin Heidelberg, 2001. http://dx.doi.org/10.1007/978-3-540-45359-8_20.

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Ananthapadmanabha, T. V. "Aerodynamic and Acoustic Theory of Voice Production." In Forensic Speaker Recognition. Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4614-0263-3_12.

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Swanson, David C. "Acoustic Data Acquisition." In Handbook of Signal Processing in Acoustics. Springer New York, 2008. http://dx.doi.org/10.1007/978-0-387-30441-0_2.

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Solé, Maria-Josep. "Acoustic and aerodynamic factors in the interaction of features." In Phonetics and Phonology. John Benjamins Publishing Company, 2009. http://dx.doi.org/10.1075/cilt.306.10sol.

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Weiland, Claus. "Introduction." In Aerodynamic Data of Space Vehicles. Springer Berlin Heidelberg, 2014. http://dx.doi.org/10.1007/978-3-642-54168-1_1.

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Weiland, Claus. "The Discipline Aerodynamics." In Aerodynamic Data of Space Vehicles. Springer Berlin Heidelberg, 2014. http://dx.doi.org/10.1007/978-3-642-54168-1_2.

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Weiland, Claus. "Classification and Project Data of Space Vehicles." In Aerodynamic Data of Space Vehicles. Springer Berlin Heidelberg, 2014. http://dx.doi.org/10.1007/978-3-642-54168-1_3.

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Weiland, Claus. "Aerodynamic Data of Non-Winged Re-entry Vehicles (RV-NW) - Capsules and Probes -." In Aerodynamic Data of Space Vehicles. Springer Berlin Heidelberg, 2014. http://dx.doi.org/10.1007/978-3-642-54168-1_4.

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Actas de conferencias sobre el tema "Aerodynamic and acoustic data"

1

Jeng, Yih-Nen, Tzung-Ming Yang, You-Chi Cheng, and Jia-Ming Huang. "Acoustic Data Analysis of Remote Control Vehicles via Fourier Sine Spectrum and Spectrogram." In 26th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-4263.

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Su, Jialin, Andrew Garmory, and Jon Carrotte. "The Aerodynamic Response of Fuel Injector Passages to Incident Acoustic Waves." In ASME Turbo Expo 2015: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/gt2015-43248.

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Modern low emission combustion systems are more prone to combustion instabilities due to operation at lean conditions. The response of the airflow passing through the injector to incident acoustic waves is therefore of interest. Airflow fluctuations can initiate, for example, perturbations in stoichiometry and velocity that are subsequently delivered into the heat release region. In the case of liquid fuelled gas turbines the atomisation process will also be affected. Such effects can lead to further unsteady heat release and the generation of acoustic waves, thereby leading to combustion inst
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3

Dykas, Slawomir, Wlodzimierz Wroblewski, and Tadeusz Chmielniak. "Aerodynamic Noise Assessment Using CFD/CAA Technique." In ASME Turbo Expo 2008: Power for Land, Sea, and Air. ASMEDC, 2008. http://dx.doi.org/10.1115/gt2008-50140.

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In the presented paper a numerical method for aerodynamic noise assessment on the basis of unsteady mean flow field data has been presented. This method belongs to the very wide family of so called hybrid CFD/CAA methods. In described method for calculations of the acoustic fluctuations a solution of full non-linear Euler equations is used. The Euler equations are solved with the use of numerical scheme with third order accuracy in space and time. The presented method is numerically decoupled with CFD solution, so that the information about mean unsteady flow field can be obtained using arbitr
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Buffum, Daniel H., and Sanford Fleeter. "Effect of Wind Tunnel Acoustic Modes on Linear Oscillating Cascade Aerodynamics." In ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1993. http://dx.doi.org/10.1115/93-gt-149.

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The aerodynamics of a biconvex airfoil cascade oscillating in torsion is investigated using the unsteady aerodynamic influence coefficient technique. For subsonic flow and reduced frequencies as large as 0.9, airfoil surface unsteady pressures resulting from oscillation of one of the airfoils are measured using flush-mounted high-frequency-response pressure transducers. The influence coefficient data are examined in detail and then used to predict the unsteady aerodynamics of a cascade oscillating at various interblade phase angles. These results are correlated with experimental data obtained
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5

Karstadt, Sascha, Michael Hess, Berthold Matyschok, and Peter F. Pelz. "The Influence of Tip Clearance on the Acoustic and Aerodynamic Characteristics of Fans." In ASME Turbo Expo 2010: Power for Land, Sea, and Air. ASMEDC, 2010. http://dx.doi.org/10.1115/gt2010-22082.

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In addition to developing fans as aerodynamically efficient as possible, acoustic optimization gains more and more importance for the purpose of reducing fan noise exposure. In order to combine good aerodynamic properties with a silent fan, this experimental research investigates the acoustic and aerodynamic characteristics of an axial fan. In this case, a fan with skewed blades is tested in view of its aerodynamic efficiency and noise exposure in dependence on its tip clearance and stagger angle. For this purpose, six different stagger angles and five tip clearance gaps per angle were measure
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Pan, Minghao, Paul Petrie-Repar, Hans Mårtensson, Tianrui Sun, and Tobias Gezork. "Determination of Aerodynamic Damping at High Reduced Frequencies." In ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/gt2018-75294.

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In turbomachines, forced response of blades is blade vibrations due to external aerodynamic excitations and it can lead to blade failures which can have fatal or severe economic consequences. The estimation of the level of vibration due to forced response is dependent on the determination of aerodynamic damping. The most critical cases for forced response occur at high reduced frequencies. This paper investigates the determination of aerodynamic damping at high reduced frequencies. The aerodynamic damping was calculated by a linearized Navier-Stokes flow solver with exact 3D non-reflecting bou
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Lee, S., H. J. Kim, W. S. Song, and K. W. Ahn. "Aero-Acoustic Design of Fan Using Inverse Method." In ASME/JSME 2003 4th Joint Fluids Summer Engineering Conference. ASMEDC, 2003. http://dx.doi.org/10.1115/fedsm2003-45119.

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A multi-dimensional inverse algorithm was developed to design low noise fan. In this approach, mean-line analysis, 3-D CAD, automatic grid generation method, and CFD solver can be integrated with aero-acoustic inverse design method. The overall sound pressure level distributions obtained from specified sets of unsteady blade loading distribution serve input data to the multi-dimensional acoustic inverse module, and may be used to design optimal geometry to satisfy the aerodynamic and aero-acoustic performance. To execute an effective inversion of non-minimum phase system, SVD is introduced. Wi
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Luo, Bo, Wuli Chu, Wei Dong, and Xiangyi Chen. "Aerodynamic Characteristics and Noise Analysis of a Low-Speed Axial Fan." In ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/gt2018-76079.

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Axial fans are widely used in modern industry and new regulations and stringent environmental concerns are prompting manufacturer to design efficient low-noise axial fans. This paper is focused on improving the aerodynamic performances and reducing the tonal noise at BPF and its harmonics by the optimum choice of lean-swept blade and the stacking line for the low-speed axial fan. The aerodynamic characteristics of the axial fan with a shroud are explored by CFD with ANASYS CFX. A hybrid method, SST turbulence model for flow and FW-H equation for acoustics, is chosen to predict the radiated noi
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Lee, Chan, and Hyun Gwon Kil. "An Aero-Acoustic Performance Prediction Method of Sirocco Fan." In ASME 2010 3rd Joint US-European Fluids Engineering Summer Meeting collocated with 8th International Conference on Nanochannels, Microchannels, and Minichannels. ASMEDC, 2010. http://dx.doi.org/10.1115/fedsm-icnmm2010-31040.

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A design-analysis method of Sirocco fan is developed for constructing 3-D impeller and scroll geometries, and for predicting both the aerodynamic performance and the noise characteristics of the designed fan. The aerodynamic blading design of fan is conducted by blade angle, camber line determinations and airfoil thickness distribution, and then the scroll geometry of fan is designed by using logarithmic spiral. The aerodynamic performance of designed fan is predicted by the mean line analysis with flow blockage, slip and pressure loss correlations. Based on the predicted performance data, fan
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Rulik, Sebastian, Slawomir Dykas, and Wlodzimierz Wroblewski. "Modeling of Aerodynamic Noise Using Hybrid SAS and DES Methods." In ASME Turbo Expo 2010: Power for Land, Sea, and Air. ASMEDC, 2010. http://dx.doi.org/10.1115/gt2010-22696.

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The purpose of the presented studies is to compare simple and fast CFD methods based on the unsteady Reynolds-Averaged Navier-Stokes equations (uRANS) with the so called hybrid uRANS/LES methods like Detached Eddy Simulation (DES) and Scale Adaptive Simulation (SAS) implemented in the commercial code ANSYS CFX. The goal of this comparison is to find an efficient and relatively fast method for both the flow dynamic and aerodynamic noise prediction in the near and far field, which would be suitable for engineering applications. The CFD calculations were carried out using the commercial code ANSY
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Informes sobre el tema "Aerodynamic and acoustic data"

1

Bergès, B. J. P., and S. Sakinan. Analysis of ancillary acoustic data during acoustic trawl surveys. Stichting Wageningen Research, Centre for Fisheries Research (CVO), 2020. http://dx.doi.org/10.18174/522177.

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Matzner, Shari, Joshua R. Myers, Adam R. Maxwell, and Mark E. Jones. NW-MILO Acoustic Data Collection. Office of Scientific and Technical Information (OSTI), 2010. http://dx.doi.org/10.2172/989033.

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Newcomb, J., and R. A. Wagstaff. Development of Sensible Acoustic Data Bases. Defense Technical Information Center, 1990. http://dx.doi.org/10.21236/ada230699.

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Hodgkiss, W. S., and H. C. Song. Environmental Fluctuations and Acoustic Data Communications. Defense Technical Information Center, 2014. http://dx.doi.org/10.21236/ada617709.

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Dahl, Peter H., and William J. Plant. Analysis of Simultaneous Acoustic/Microwave Data. Defense Technical Information Center, 2002. http://dx.doi.org/10.21236/ada626255.

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Moore, T. K. Initial borehole acoustic televiewer data processing algorithms. Office of Scientific and Technical Information (OSTI), 1988. http://dx.doi.org/10.2172/7028219.

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Worcester, Peter F., James A. Mercer, and Robert C. Spindel. Ocean Acoustic Observatories: Data Analysis and Interpretation. Defense Technical Information Center, 1997. http://dx.doi.org/10.21236/ada628417.

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Worcester, Peter F., James A. Mercer, and Robert C. Spindel. Ocean Acoustic Observatories: Data Analysis and Interpretation. Defense Technical Information Center, 1999. http://dx.doi.org/10.21236/ada629597.

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Hehman, C. S. Empirical modeling of electromagnetic acoustic transducer data. National Institute of Standards and Technology, 1999. http://dx.doi.org/10.6028/nist.ir.5087.

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Smith, Kevin B. Comparative Beamforming and Acoustic Inversion Studies Employing Acoustic Vector Data in Shallow Water. Defense Technical Information Center, 2007. http://dx.doi.org/10.21236/ada569148.

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