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  • Comparative Studies. Non-European Languages/Literatures  (10)
  • 1
    Online Resource
    Online Resource
    Acoustical Society of America (ASA) ; 2016
    In:  Journal of the Acoustical Society of America Vol. 140, No. 4_Supplement ( 2016-10-01), p. 3043-3043
    In: Journal of the Acoustical Society of America, Acoustical Society of America (ASA), Vol. 140, No. 4_Supplement ( 2016-10-01), p. 3043-3043
    Abstract: Strong acoustic waves emitted from rocket plume might damage to rocket payloads because rocket payloads consist of fragile structure. Therefore, it is important to predict acoustic directivity and reduce its intensity level. In this study, we conduct experiments of supersonic jet flows and investigate an influence of the nozzle geometry on acoustic waves by means of Schlieren method and microphone measurement. Three different nozzles are examined: a conical nozzle, a convergent-divergent nozzle (referred as C-D nozzle), and a tab-C-D nozzle. Tabs are equipped in the nozzle inside and turbulence is generated in the tab-C-D nozzle case. The Schlieren visualization shows that the strong shock trains are observed in the potential core of the jet for the conical nozzle case, while the shock waves are relatively weak since the nozzles are in the nearly ideal expanded condition in the C-D nozzle and tab-C-D cases. The distribution of near field OASPL (over all sound pressure level) obtained by microphone measurement shows strong directivity in the downstream direction for all the cases. This directivity seems to be the Mach wave radiation. Moreover, conical nozzle cases have strong acoustic intensity level caused by shock associated noise.
    Type of Medium: Online Resource
    ISSN: 0001-4966 , 1520-8524
    RVK:
    Language: English
    Publisher: Acoustical Society of America (ASA)
    Publication Date: 2016
    detail.hit.zdb_id: 1461063-2
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  • 2
    Online Resource
    Online Resource
    Acoustical Society of America (ASA) ; 2016
    In:  Journal of the Acoustical Society of America Vol. 140, No. 4_Supplement ( 2016-10-01), p. 3097-3097
    In: Journal of the Acoustical Society of America, Acoustical Society of America (ASA), Vol. 140, No. 4_Supplement ( 2016-10-01), p. 3097-3097
    Abstract: Strong acoustic waves are generated from the rocket plumes in the supersonic jet condition. The acoustic waves are significantly affected by temperature of jets. In this study, we perform large eddy simulations of the acoustic waves generated from the hot and cold jets. The temperature ratio of chamber to ambient air is set to be 4.0 and 1.0 for the hot and cold jets, respectively. Mach waves are radiated from the region close to the nozzle exit. In the hot jet case, we confirmed that the shorter potential core length, the larger angle of Mach waves, and the higher sound pressure level, as compared with those in the cold jet case.
    Type of Medium: Online Resource
    ISSN: 0001-4966 , 1520-8524
    RVK:
    Language: English
    Publisher: Acoustical Society of America (ASA)
    Publication Date: 2016
    detail.hit.zdb_id: 1461063-2
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  • 3
    Online Resource
    Online Resource
    Acoustical Society of America (ASA) ; 2016
    In:  Journal of the Acoustical Society of America Vol. 140, No. 4_Supplement ( 2016-10-01), p. 3421-3421
    In: Journal of the Acoustical Society of America, Acoustical Society of America (ASA), Vol. 140, No. 4_Supplement ( 2016-10-01), p. 3421-3421
    Abstract: The objective of this study was to understand the sound generation of flapping wings. In particular, the structural properties of the wings were varied to assess the effects of wing flexibility on the sound generation of flapping wings. A four-wing, hummingbird-inspired flapping wing micro air vehicle (FMAV) was considered. The half wing span was approximately six centimeters and the flapping frequency was approximately 25 Hz. The sound produced by the FMAV was measured using a 1/2 inches diameter microphone in an acoustic chamber under the quiescent flow condition. Time-averaged aerodynamic forces were measured by the force and torque sensor Nano17 (ATI Industrial Automation). Results revealed the characteristics of flapping-wing sound in terms of directivity, frequency response, and attenuation. Moreover, the degree of wing deformation led to a variation in the frequency response corresponding to the maximum sound pressure level as well as time-averaged aerodynamic force, even when the flapping frequency was held constant in all the cases. All outcomes of this study would be helpful to control the sound generation of FMAVs and to develop new, silent FMAVs.
    Type of Medium: Online Resource
    ISSN: 0001-4966 , 1520-8524
    RVK:
    Language: English
    Publisher: Acoustical Society of America (ASA)
    Publication Date: 2016
    detail.hit.zdb_id: 1461063-2
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  • 4
    Online Resource
    Online Resource
    Acoustical Society of America (ASA) ; 1984
    In:  The Journal of the Acoustical Society of America Vol. 75, No. 1 ( 1984-01-01), p. 308-308
    In: The Journal of the Acoustical Society of America, Acoustical Society of America (ASA), Vol. 75, No. 1 ( 1984-01-01), p. 308-308
    Type of Medium: Online Resource
    ISSN: 0001-4966 , 1520-8524
    RVK:
    Language: English
    Publisher: Acoustical Society of America (ASA)
    Publication Date: 1984
    detail.hit.zdb_id: 1461063-2
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  • 5
    Online Resource
    Online Resource
    Acoustical Society of America (ASA) ; 1980
    In:  The Journal of the Acoustical Society of America Vol. 67, No. 2 ( 1980-02-01), p. 750-750
    In: The Journal of the Acoustical Society of America, Acoustical Society of America (ASA), Vol. 67, No. 2 ( 1980-02-01), p. 750-750
    Type of Medium: Online Resource
    ISSN: 0001-4966 , 1520-8524
    RVK:
    Language: English
    Publisher: Acoustical Society of America (ASA)
    Publication Date: 1980
    detail.hit.zdb_id: 1461063-2
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  • 6
    Online Resource
    Online Resource
    Acoustical Society of America (ASA) ; 1984
    In:  The Journal of the Acoustical Society of America Vol. 76, No. 4 ( 1984-10-01), p. 1288-1288
    In: The Journal of the Acoustical Society of America, Acoustical Society of America (ASA), Vol. 76, No. 4 ( 1984-10-01), p. 1288-1288
    Type of Medium: Online Resource
    ISSN: 0001-4966 , 1520-8524
    RVK:
    Language: English
    Publisher: Acoustical Society of America (ASA)
    Publication Date: 1984
    detail.hit.zdb_id: 1461063-2
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  • 7
    Online Resource
    Online Resource
    Acoustical Society of America (ASA) ; 1996
    In:  The Journal of the Acoustical Society of America Vol. 100, No. 4_Supplement ( 1996-10-01), p. 2763-2763
    In: The Journal of the Acoustical Society of America, Acoustical Society of America (ASA), Vol. 100, No. 4_Supplement ( 1996-10-01), p. 2763-2763
    Abstract: KDD has developed a telephone operator assisting system, which provides operators with automatic database inquiry using speech recognition. An outline of the system is described and the results of a field trial are evaluated. There have been many speech recognition systems for practical use. A fast recognition method is one of the important subjects for practical systems. For this purpose, various methods are proposed. [Sagayama et al. ‘‘New Approaches Toward Fast Speech Recognition,’’ Proc. Acoust. Soc. Jpn. 25–28 (1996) (in Japanese)]. However, it takes some frames to output recognition results after finishing speech input, because any method deals with a few 100-ms pause following speech, which is a margin to detect the speech end. Therefore, a new fast recognition method is proposed. The basic idea of this approach is to output results when inquiry keywords are decided, even before detecting the speech end. This approach makes it possible not only to reduce speech recognition time, but also to recognize speech including out-of-vocabulary words and nonspeech sounds at the end of a sentence. Evaluation results show that (1) speech recognition time was reduced 30% and (2) high recognition accuracy was achieved: 95% for only expected inputs, 92% for all inputs. Fifty percent of unexpected inputs included out-of-vocabulary words at the end of a sentence, and most of them can be recognized correctly using this method.
    Type of Medium: Online Resource
    ISSN: 0001-4966 , 1520-8524
    RVK:
    Language: English
    Publisher: Acoustical Society of America (ASA)
    Publication Date: 1996
    detail.hit.zdb_id: 1461063-2
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  • 8
    Online Resource
    Online Resource
    Acoustical Society of America (ASA) ; 1978
    In:  The Journal of the Acoustical Society of America Vol. 64, No. S1 ( 1978-11-01), p. S102-S103
    In: The Journal of the Acoustical Society of America, Acoustical Society of America (ASA), Vol. 64, No. S1 ( 1978-11-01), p. S102-S103
    Abstract: Formation of corrugation on the loudspeaker cones has been commonly used for a long time to control vibrational characteristics of the cones, however, no practical formula for designing the corrugation has ever been developed. The authors have developed an approximate formula for the corrugation design with the aid of the Finite Element Method. Since the corrugation provides a lower stiffness to the loudspeaker cone at its lumped portion, the effectiveness of the corrugation depends upon the stiffness ratio between the corrugation and the cone. Two equations are introduced to obtain the stiffness ratio. One is for the effective stiffness of corrugation which involves the material, the shape, and the dimensions of the corrugation, with the ratio of the corrugation curvature to the width as a parameter and the other is for the effective stiffness of cone as a function of its shape. The ratio of the two equations gives a practical formula for corrugation design. Graphical displays of the cone vibration obtained by using the F.E.M. are close to authors' expectation. The effects of corrugation on the cone vibration and on the on-axis frequency responses are also discussed.
    Type of Medium: Online Resource
    ISSN: 0001-4966 , 1520-8524
    RVK:
    Language: English
    Publisher: Acoustical Society of America (ASA)
    Publication Date: 1978
    detail.hit.zdb_id: 1461063-2
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  • 9
    Online Resource
    Online Resource
    Acoustical Society of America (ASA) ; 1984
    In:  The Journal of the Acoustical Society of America Vol. 75, No. 4 ( 1984-04-01), p. 1319-1320
    In: The Journal of the Acoustical Society of America, Acoustical Society of America (ASA), Vol. 75, No. 4 ( 1984-04-01), p. 1319-1320
    Type of Medium: Online Resource
    ISSN: 0001-4966 , 1520-8524
    RVK:
    Language: English
    Publisher: Acoustical Society of America (ASA)
    Publication Date: 1984
    detail.hit.zdb_id: 1461063-2
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  • 10
    Online Resource
    Online Resource
    Acoustical Society of America (ASA) ; 2009
    In:  The Journal of the Acoustical Society of America Vol. 126, No. 6 ( 2009-12-01), p. 3020-3027
    In: The Journal of the Acoustical Society of America, Acoustical Society of America (ASA), Vol. 126, No. 6 ( 2009-12-01), p. 3020-3027
    Abstract: Three different techniques for evaluating the absorption coefficient of sound absorbing materials in free field conditions are discussed. One technique measures the acoustic impedance at one point nearby a specimen, the other two techniques evaluate the impedance from the transfer function of two sound pressures and two particle velocities at two points. These are called “PU-method,” “PP-method,” and “UU-method,” respectively. An iterative algorithm to estimate the acoustic impedance of the locally reactive specimen in the spherical wave field is also applied. First, the effect of receiver positions, specimen areas, and source heights to the measured normal absorption coefficient is investigated by the boundary element method. According to these investigations, the PU-method is most stable against the effect of specimen area, and the UU-method is easily affected by that effect. Closer source to the specimen distance is advantageous for the signal to noise ratio of these measurement techniques, but correction for the effect of the spherical wave field has to be applied. As a finding, the iterative algorithm works for all of three techniques. Finally, the PU-method is applied experimentally with a pressure-velocity sensor and a loudspeaker in a hemi-anechoic room. As a result, the calculated results have been verified.
    Type of Medium: Online Resource
    ISSN: 0001-4966 , 1520-8524
    RVK:
    Language: English
    Publisher: Acoustical Society of America (ASA)
    Publication Date: 2009
    detail.hit.zdb_id: 1461063-2
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