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FRIDAY MORNING, 20 MAY 2005 REGENCY E, 8:30 A.M. TO 12:00 ...

FRIDAY MORNING, 20 MAY 2005 REGENCY E, 8:30 A.M. TO 12:00 ...

FRIDAY MORNING, 20 MAY 2005 REGENCY E, 8:30 A.M. TO 12:00 ...

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5aPP24. Utilizing different channels for multiple inputs in cochlear<br />

implant processing. Bom Jun Kwon Cochlear Americas, 4<strong>00</strong><br />

Inverness Pkwy, Ste. 4<strong>00</strong>, Englewood, CO 801<strong>12</strong>, bjkwon@gmail.com<br />

While cochlear implants successfully provide auditory sensation for<br />

deaf people, speech understanding through the device is compromised<br />

when there is a background noise or competing sounds, partly due to<br />

implant users’ reduced ability in auditory grouping. The present study<br />

investigates whether providing multiple streams of input on different channels<br />

would facilitate auditory grouping, thereby assisting speech understanding<br />

in competing sounds. In acoustic hearing, presenting two streams<br />

of input such as speech and noise in spectrally separate channels generally<br />

facilitates grouping; however, in electric hearing it is difficult to predict<br />

and separating them could lead to a negative result, because channel<br />

interactions inferred from the excitation patterns are severe and the actual<br />

amount of electric current for the noise delivered to the cochlea would be<br />

much higher for a given SNR, therefore contaminating the target more<br />

effectively. Results from consonant identification measured in a variety of<br />

speech/noise conditions same/different channels indicate that speech understanding<br />

generally improves with separate channels, implying that implant<br />

users appear to extract speech information on the basis of spatial<br />

channel separation, easily overcoming the distracter from the adjacent<br />

channels with higher intensity. This also proposes a new measure of channel<br />

interactions based on auditory grouping.<br />

<strong>FRIDAY</strong> <strong>MORNING</strong>, <strong>20</strong> <strong>MAY</strong> <strong>20</strong>05<br />

PLAZA B, 9:<strong>00</strong> A.M. <strong>TO</strong> <strong>12</strong>:<strong>00</strong> NOON<br />

Session 5aSA<br />

Structural Acoustics and Vibration: General Vibration: Modeling, Propagation, Dissipation and Control<br />

Linda P. Franzoni, Chair<br />

Dept. of Mechanical Engineering and Material Science, Duke Univ., Durham, NC 27708-0<strong>30</strong>0<br />

Contributed Papers<br />

9:<strong>00</strong><br />

5aSA1. Time reversal in heterogeneous flexural beams. Dany<br />

Francoeur and Alain Berry Dept. Gen. Mecanique, Universite de<br />

Sherbrooke, 25<strong>00</strong> boul. de l’Universite, Sherbrooke, QC, Canada J1K 2R1,<br />

Alain.Berry@USherbrooke.ca<br />

Time reversal of acoustic and structure-borne waves has been explored<br />

in recent years mostly for ultrasound and for nondispersive propagation,<br />

that is under frequency-independent wave velocity. In contrast, the case of<br />

time reversal in flexural beams presented here involves dispersive propagation,<br />

and is carried for frequencies below 5 kHz. The study has been<br />

started with analytical time reversal simulations in infinite homogeneous<br />

or heterogeneous beams comprising point-mass scatterers. Experiments<br />

have also been realized on a5mbeam with anechoic terminations and<br />

under transverse impact excitation. The time-reversal mirror was made of<br />

several thin piezoceramic elements bonded on the beam to sense the impulse<br />

response of the structure and re-emit its time-reversed image. The<br />

experimental results are in good agreement with the analytical results, and<br />

show that time spreading due to dispersive propagation of bending waves<br />

is successfully compensated by the time reversal operation. The presentation<br />

will illustrate the main results of the simulations and a comparison<br />

with the experiments.<br />

9:15<br />

5aSA2. Medium frequency vibration modeling of cracked plates using<br />

hierarchical trigonometric functions. Jérôme Pinsonnault, Patrice<br />

Masson, Philippe Micheau GAUS, Mech. Eng. Dept., Université de<br />

Sherbrooke, Sherbrooke, QC, Canada J1K 2R1,<br />

Patrice.Masson@USherbrooke.ca, and Nezih Mrad Defence R&D<br />

Canada, Dept. of Natl. Defence, Ottawa, ON, Canada K1A 0K2<br />

A modeling tool is proposed to describe the vibration behavior of<br />

pristine and damaged plates in the medium frequency range below 10<br />

kHz. This tool is intended to provide a platform for the development and<br />

assessment of damage detection algorithms for aircraft structural health<br />

monitoring applications. The proposed analytical model employs a Hierarchical<br />

Trigonometric Function Set HTFS to characterize homogeneous<br />

plates with through cracks. This approach takes advantage of the very high<br />

order of stability of the HTFS O. Beslin and J. Nicolas, J. Sound Vib.<br />

<strong>20</strong>2, 633–655 1997 to approximate the effects of a small crack in a<br />

plate for all combinations of classical boundary conditions e.g., CFSC,<br />

CCFF, FSFS. The model is first presented and then assessed for healthy<br />

and cracked CCCC plates with eigenvalues and eigenmodes presented in<br />

the literature. For a healthy square plate, numerical results provide good<br />

agreement up to the 1<strong>00</strong>0th mode while, for a cracked rectangular plate,<br />

good agreement is obtained up to the 3rd mode, corresponding to the<br />

highest mode order available in the literature. Wave propagation simulation<br />

obtained from HTFS shows the scattering around the cracks in the<br />

plates. Experimental validation of the model is conducted both in frequency<br />

and time domains for healthy and cracked plates. Work supported<br />

by the Consortium for Research and Innovation in Aerospace in Quebec<br />

CRIAQ and Defence R&D Canada.<br />

9:<strong>30</strong><br />

5aSA3. An exact analytical expression of the shear coefficient in the<br />

Mindlin plate equation. Andrew Hull Code 82<strong>12</strong>, Naval Undersea<br />

Warfare Ctr., Newport, RI 02841, hullaj@npt.nuwc.navy.mil<br />

This paper derives an exact analytical expression of the shear coefficient<br />

in the Mindlin plate equation for a plate of infinite extent. The equation<br />

of motion derived from the Mindlin plate equation is set equal to the<br />

equation of motion derived from the thick plate equation, and the result is<br />

a closed-form expression of the shear coefficient at all wave numbers and<br />

frequencies. A numerical example is included to illustrate the variation of<br />

the shear coefficient. It is shown that the shear coefficient is extremely<br />

dependent on wave number and only slightly dependent on frequency.<br />

Shear coefficients derived in other work are compared favorably to the<br />

values calculated by this new method at the plate flexural wave response.<br />

Work funded by the Office of Naval Research.<br />

9:45<br />

5aSA4. Structural acoustic control of plates with variable boundary<br />

conditions. Robert L. Clark, Joseph D. Sprofera Dept. of Mech. Eng.<br />

and Mater. Sci., Duke Univ., Box 90<strong>30</strong>0, Durham, NC 27708-0<strong>30</strong>0, Gary<br />

P. Gibbs, and Ran H. Cabell NASA Langley Res. Ctr., Structural Acoust.<br />

Branch<br />

A method for optimizing a structural acoustic control system with<br />

respect to potential variations in plate boundary conditions is provided.<br />

The assumed modes method is used to build a plate model with varying<br />

levels of rotational boundary stiffness to span a range of possible boundary<br />

conditions which can be used to capture uncertainty in the model. A trans-<br />

5a FRI. AM<br />

2601 J. Acoust. Soc. Am., Vol. 117, No. 4, Pt. 2, April <strong>20</strong>05 149th Meeting: Acoustical Society of America 2601

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