Background: A previous experiment with 70 interrupted monosyllabic words demonstrated that recognition performance was influenced by the location of an interruption pattern (Wilson, 2014). The interruption paradigm (10 interruptions/sec, 50% duty cycle periodic interruption) was referenced to word onset. The words were interrupted such that alternate 50-msec segments were parsed to separate files. In the 0-msec condition the first on-segment coincided with the word onset, whereas in the 50-msec condition the first on-segment occurred 50 msec after word onset. The 0- and 50-msec conditions were complementary halves. Recognition performance by young listeners was 19% better on the 0-msec condition (86%) than on the 50-msec condition (68%); there were a minority number of words on which the results were just the opposite. A second study using the same interruption paradigm but 300 different words reported similar relations, with 63% correct recognition on the 0-msec condition and 48% on the 50-msec condition (Wilson and Irish, 2015). Both studies suggest the importance that the first 50 msec of the target word has on intelligibility. Purpose: To define in detail the effects that interruption patterns have on word recognition as the interruption pattern was incremented with reference to word onset from 0 to 90 msec in 10-msec steps. Research Design: A repeated-measures design with ten interruption patterns (onset conditions). Study Sample: Twenty-four young listeners (19-29 yr) with normal hearing for pure tones participated in this study. Data Collection and Analyses: Seventy consonant-nucleus-consonant words formed the corpus of materials with 25 additional words used for practice. For each participant, the 700 stimuli (70 words by ten onset conditions) were interrupted (10 interruptions/sec; 50% duty cycle), randomized, and recorded on compact disc in 28, 25-word tracks. Results: The overall mean recognition performance was 80.4% with mean performances for the ten conditions ranging from 73.0% (50-msec condition) to 87.7% (90-msec condition). The mean recognition performances changed systematically, decreasing from the 0-msec condition to the 50-msec condition and then increasing to the 90-msec condition, which formed a U-shaped function of the means. Of the 45 mean paired comparisons (post hoc t-tests with Bonferroni corrections), there were 17 significant differences at the p ≤ 0.001 level, increasing to 31 significant differences when the significance level was increased to the p ≤ 0.01 level. Visual inspection of the 70-word performance functions revealed that 32 words had flat functions, 34 words had U-shaped functions, two functions were rising, one was an inverted V-shape, and one was irregular. Conclusions: First, some words (utterances of those words) were immune to any differential effects of the ten interruption patterns. These words with flat performance functions constituted 46% of the word corpus. Second, 49% of the words exhibited U-shaped performance functions that were always systematic, going from maximum to minimum and back to maximum. These words were thought to be more dependent on the initial consonant to attain maximum performance. The conclusion is that some words are not affected by the location of the interruption pattern (those with flat functions) whereas other words are substantially affected (those with U-shaped functions).

Background: Two previous experiments from our laboratory with 70 interrupted monosyllabic words demonstrated that recognition performance was influenced by the temporal location of the interruption pattern. The interruption pattern (10 interruptions/sec, 50% duty cycle) was always the same and referenced word onset; the only difference between the patterns was the temporal location of the onand off-segments of the interruption cycle. In the first study, both young and older listeners obtained better recognition performances when the initial on-segment coincided with word onset than when the initial on-segment was delayed by 50 msec. The second experiment with 24 young listeners detailed recognition performance as the interruption pattern was incremented in 10-msec steps through the 0-To 90-msec onset range. Across the onset conditions, 95% of the functions were either flat or U-shaped. Purpose: To define the effects that interruption pattern locations had on word recognition by older listeners with sensorineural hearing loss as the interruption pattern incremented, re: Word onset, from 0 to 90 msec in 10-msec steps. Research Design: A repeated-measures design with ten interruption patterns (onset conditions) and one uninterruption condition. Study Sample: Twenty-four older males (mean = 69.6 yr) with sensorineural hearing loss participated in two 1-hour sessions. The three-frequency pure-Tone average was 24.0 dB HL and word recognition was $80% correct. Data Collection and Analyses: Seventy consonant-vowel nucleus-consonant words formed the corpus of materials with 25 additional words used for practice. For each participant, the 700 interrupted stimuli (70 words by 10 onset conditions), the 70 words uninterrupted, and two practice lists each were randomized and recorded on compact disc in 33 tracks of 25 words each. Results: The data were analyzed at the participant and word levels and compared to the results obtained earlier on 24 young listeners with normal hearing. The mean recognition performance on the 70 words uninterrupted was 91.0% with an overallmean performance on the ten interruption conditions of 63.2% (range: 57.9-69.3%), compared to 80.4% (range: 73.0-87.7%) obtained earlier on the young adults. The best performances were at the extremes of the onset conditions. Standard deviations ranged from 22.1% to 28.1% (24 participants) and from 9.2% to 12.8% (70 words). An arithmetic algorithm categorized the shapes of the psychometric functions across the ten onset conditions.With the older participants in the current study, 40% of the functions were flat, 41.4% were U-shaped, and 18.6% were inverted U-shaped, which compared favorably to the function shapes by the young listeners in the earlier study of 50.0%, 41.4%, and 8.6%, respectively. There were two words on which the older listeners had 40% better performances. Conclusion: Collectively, the data are orderly, but at the individual word or participant level, the data are somewhat volatile, which may reflect auditory processing differences between the participant groups. The diversity of recognition performances by the older listeners on the ten interruption conditions with each of the 70 words supports the notion that the term hearing loss is inclusive of processes well beyond the filtering produced by end-organ sensitivity deficits.

En phase d’approche, le bruit rayonné par l’entrée d’air des turboréacteurs est principalement dû aux interactions entre le rotor et le stator. Cependant les ondes de choc (ou ondes en N) générées par le rotor en régime transsonique peuvent devenir une source de bruit dominante durant le décollage et la montée de l’appareil. L’étude des ondes en N nécessite de se concentrer sur deux processus majeurs : 1) la génération des chocs par un rotor parfait (dont toutes les aubes sont identiques) et par un rotor réel (en tenant compte des irrégularités géométriques des aubes), et 2) la propagation de ces ondes en N à travers la nacelle, produisant du bruit dont le spectre se compose des harmoniques de la fréquence de passage des aubes pour un rotor régulier, et des harmoniques aux fréquences multiples de la rotation du rotor (FMR) pour un rotor irrégulier. Plusieurs approches analytiques et numériques ont été développées durant les 40 dernières années.Cette thèse relate dans un tout premier temps les principales théories de la propagation des ondes de choc ainsi que les modèles majeurs de génération de FMR. Une attention particulière est portée sur les liens entre les équations générales de la mécanique des fluides et ces modèles de propagation non linéaire afin de mettre en évidence les différentes hypothèses formulées dans ces modèles. Dans un deuxième temps, les principales méthodes semi-analytiques de génération et de propagation des chocs seront évaluées et comparées en les appliquant à des configurations de turboréacteurs. En outre, un nouveau modèle de génération de FMR basé sur des considérations géométriques est élaboré par l’intermédiaire d’une campagne d’essais comportant d’une part des mesures de signaux de pression dans la nacelle et d’autre part les mesures des angles de calage des aubes pendant le fonctionnement du moteur. Le deuxième volet de la thèse concerne le développement d’une méthodologie de simulation numérique basée sur l’utilisation du code elsA de l’ONERA en résolvant les équations d’Euler (approche CAA). L’objectif de cette approche est de s’affranchir des limitations des modèles de propagation semi-analytiques et de tenir compte de la géométrie réelle de la nacelle ainsi que d’un écoulement réaliste. Des ondes de choc régulières et irrégulières sont directement injectées dans un plan proche de la soufflante et se propagent en remontant l’écoulement. Ces ondes de choc sont injectées par l’intermédiaire d’une condition limite de non-réflexion qui nécessite d’imposer le champ conservatif. La signature des chocs peut provenir d’un RANS, de mesures ou d’un signal analytique. Étant donné que les mesures ou le signal théorique ne permettent d’obtenir que la pression, une méthode de reconstruction du champ conservatif à partir des variations de pression induites par le choc a été élaborée. Cette méthode d’injection est tout d’abord appliquée à un conduit annulaire infiniment mince et validée par la méthode de propagation semi-analytique de McAlpine & Fisher. Ensuite, les effets de propagation 3D sont étudiés en augmentant l’épaisseur du conduit. Enfin, la méthode CAA est appliquée à des configurations de turboréacteurs modernes et des ondes de choc régulières et irrégulières sont propagées numériquement. Les résultats sont comparés aux solutions RANS ainsi qu’aux mesures disponibles. / Whereas the sound radiated from the inlet of turbofans is mainly due to rotor–stator interactions in approach flight, the shock waves (or N-waves) emitted by the rotor at transonic rotation speeds can be a dominant noise source during takeoff and climb. The study of N-waves needs to take account of two main processes: 1) the generation of N-waves for a perfect rotor (in which all blades are identical) and for a real rotor (considering small geometrical blade dispersion), and 2) the N-wave propagation through the inlet duct producing the blade passing harmonics for a perfect rotor, and the multiple pure tones (harmonics of the rotation frequency) for a real rotor. Several analytical and numerical approaches have been investigated for the past 40 years.This thesis first intends to relate the main propagation theories and to address the foremost MPT generation method hypotheses. The links between fluid dynamics equations and practical non-linear theories currently adopted are emphasized and discussed. In a second step, the main relevant semi-analytical methods are cross-checked by applying them to representative turbofan configurations. Moreover, a novel model of irregular N-wave generation based on geometrical considerations is investigated thanks to test data related to in-duct pressure signatures and blade stagger angle measurements during the engine operation. Then, a second part of the work investigates a numerical strategy based on elsA ONERA code, solving the full Euler’s equations (CAA approach). The objective is to prevent from the limitations of 2D analytical models and to take into account actual inlet geometry and realistic convection flow. Regular and non-regular shock waves are directly injected in a plane close to the fan and propagated through the inlet. These shock waves are injected through a non-reflective boundary condition which requires the conservative field. The initial shock description near the fan is provided either by a RANS computation or by experiment, or else from analytical model. As experiment or analytical signals only provide pressure signatures, a theory is set up to re-built the whole conservative field from the basis of a pressure shockwave. This injection method is firstly applied on an infinitely narrow annular duct and validated through the comparison with the McAlpine & Fisher analytical method. Then, the 3D propagation effects are pointed out by increasing the duct height. Finally, the CAA method is applied on actual intake geometry of modern turbofan demonstrators, and propagation of regular and irregular shock-waves are simulated. The numerical results are compared to RANS solutions and to available measurements.

Le bruit généré par la détente d'un écoulement sous pression à travers des plaques multi-perforées ou des diaphragmes est étudié expérimentalement. Cette analyse est menée sur deux configurations géométriques distinctes dans lesquelles la plaque perforée est placée à la sortie d'un conduit cylindrique (configuration de jet libre) ou à l'intérieur de celui-ci (configuration de jet confiné).Dans un premier temps, une étude paramétrique acoustique est effectuée pour ces deux configurations en variant les caractéristiques géométriques des plaques perforées et les points de fonctionnement dans des régimes subsoniques et supersoniques. Les différentes sources de rayonnement pouvant apparaitre sur de tels systèmes de détente, sont alors identifiées. Par ailleurs, les effets acoustiques de chacun des paramètres géométriques sont mis en lumière, offrant ainsi une aide à la conception silencieuse de tels systèmes. Dans un second temps, l'intérêt est porté sur l'analyse de la composante à large bande dominante: le bruit de mélange. Cette étude est menée sur la configuration de jet libre et s'appuie sur des visualisations strioscopiques ainsi que sur des mesures de vélocimétrie par image de particules couplées à des acquisitions acoustiques en champ lointain. Dans le cas des diaphragmes, les différents résultats mettent en évidence des mécanismes sources du bruit de mélange similaires à ceux observés dans la littérature pour les jets isolés issus de tuyères. Le rayonnement à l'aval, dominant, est généré par l'interaction de grosses structures turbulentes cohérentes à la fin du cône potentiel du jet, tandis que dans les autres directions, le bruit est généré par la turbulence de petite échelle dans les couches de cisaillement du jet.Pour les plaques multi-perforées, des mécanismes comparables sont également identifiés. Néanmoins, selon la géométrie de ces plaques, deux zones sources distinctes du rayonnement aval sont identifiées favorisant l'apparition de deux bosses dans les spectres en champ lointain. Dans le cas de perforations éloignées, la bosse à plus haute fréquence domine le spectre aval et l'interaction des grosses structures turbulentes se produit au niveau de la fin du cône potentiel des jets. Lorsque les perforations sont en revanche proches, c'est la bosse à basse fréquence qui domine et l'interaction des grosses structures turbulentes cohérentes semble se produire près de la fin du cône potentiel du gros jet équivalent formé à l'aval à partir du mélange de l'ensemble des jets issus des perforations. Dans les autres directions, l'espacement des perforations joue également un rôle important sur le rayonnement acoustique, du fait d'une interaction plus ou moins rapide des jets entre eux. Cela a alors pour effet de modifier les zones de cisaillement et en conséquence le rayonnement acoustique de la même manière que dans la direction aval. / The noise generated by the expansion of a pressurized flow through multi-perforated plates or diaphragms is experimentally investigated. The analysis is conducted on two distinct geometrical configurations in which the perforated plate is placed at the outlet of (free jet configuration) or inside (ducted jet configuration) a cylindrical duct.Firstly, an acoustic parametric study is carried out on these two configurations for various perforated plate geometries and for a number of operating points ranging from subsonic to supersonic. The different acoustic sources that can arise from such systems are thus identified. Furthermore, the effect of each geometrical parameter onto the radiated sound field is highlighted, thus providing guidelines for the silent design of such pressure release devices.In a second step, the focus is on the dominant broadband component, that is, the mixing noise. This part of the study is dedicated to the free jet configuration and is based on Schlieren imaging, as well as on Particle Image Velocimetry measurements, both coupled far-field sound measurements.In the diaphragm cases, the aerodynamic results show that the source mechanisms are similar to those reported in the literature about isolated jets from conventional nozzles. The downstream radiation is generated by the interaction of large coherent structures at the end of the jet potential core, while in the other directions it is generated by the small-scale turbulence from the shear layer.For multi-perforated plates, comparable mechanisms are also observed. However, depending on the plate geometry, two distinct source regions contributing to the downstream radiation are identified. They explain the presence of two broadband humps in the far-field spectra. In the case of widely spaced perforations, the higher frequency hump in the downstream spectrum increases and the interaction of the large turbulent structures occurs mainly at the end of the potential core of the small jets issuing the perforations. Conversely, when these perforations are close to each other, the small jets rapidly merge into a single larger one that has a longer potential core. As a result, larger coherent structures interact downstream of the small jet mixing region and therefore, a low-frequency hump dominates the downstream spectrum. In the other directions, the perforation spacing has also a significant impact on the acoustic radiation, due to a more or less rapid interaction of the jets. Consequently, the turbulence, as well as the shear zones of the various mixing layers, are modified. The geometric parameters thus have similar effects on the cross-stream as on the downstream radiation.

No description available.