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Scientific and Technical Aerospace Reports Volume 38 July 28, 2000

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important conclusion is that for subsonic turbulent flows, each structural mode radiates sound independently. A suitable strategy<br />

for the active structural acoustic control of the sound power transmitted through the panel would thus be independent feedback<br />

control of each structural mode in the low-frequency domain. It is also shown, however, that independent control of the panel’s<br />

radiation modes is also possible, <strong>and</strong> that this could provide a more efficient control strategy, since a smaller number of radiation<br />

modes than structural modes needs to be controlled for a given level of performance.<br />

Author<br />

Active Control; Mathematical Models; Panels; Turbulent Boundary Layer; Aircraft Noise; Harmonic Excitation; Harmonic<br />

Radiation<br />

<strong>2000</strong>0066625 Department of the Navy, Washington, DC USA<br />

Phase Fluctuation Enhanced Adaptive Processor<br />

Wagstaff, Ronald A., Inventor; Mobbs, Jackson A., Inventor; Feb. 04, <strong>2000</strong>; 31p; In English<br />

Patent Info.: Filed 4 Feb. <strong>2000</strong>; US-Patent-Appl-SN-09,498,348<br />

Report No.(s): AD-D019714; No Copyright; Avail: Issuing Activity (Defense <strong>Technical</strong> Information Center (DTIC)), Microfiche<br />

The invention uses phase fluctuations in each frequency bin to modify the exponents of pressure amplitudes (or power magnitudes)<br />

for each successive realization of a signal. As the magnitudes of the phase fluctuations decrease (i.e., signal has small magnitudes<br />

<strong>and</strong> the noise has large ones), the exponents increase. The modified pressures are summed <strong>and</strong> averaged. The resulting<br />

average is then raised to an exponent that is the average of the exponents of the individual pressures (or power magnitudes). All<br />

individual exponents <strong>and</strong> the averaged exponent in each bin are preferably bounded between optimal values of 2 <strong>and</strong> -4. The exponents<br />

will be negative for noise (attenuation), <strong>and</strong> in between for clutter signals.<br />

DTIC<br />

Signal Processing; Sonar; Noise Reduction; Underwater Acoustics; R<strong>and</strong>om Noise<br />

<strong>2000</strong>0067667 Georgia Inst. of Tech., Acoustics <strong>and</strong> <strong>Aerospace</strong> Technologies Branch, Atlanta, GA USA<br />

Active Control of Liner Impedance by Varying Perforate Orifice Geometry<br />

Ahuji, K. K., Georgia Inst. of Tech., USA; Gaeta, R. J., Jr., Georgia Inst. of Tech., USA; Mar. 31, <strong>2000</strong>; 206p; In English<br />

Contract(s)/Grant(s): NAG1-1734<br />

Report No.(s): GTRI-A5004/<strong>2000</strong>-1; No Copyright; Avail: CASI; A10, Hardcopy; A03, Microfiche<br />

The present work explored the feasibility of controlling the acoustic impedance of a resonant type acoustic liner. This was<br />

accomplished by translating one perforate over another of the same porosity creating a totally new perforate that had an intermediate<br />

porosity. This type of adjustable perforate created a variable orifice perforate whose orifices were non-circular. The key objective<br />

of the present study was to quantify, the degree of attenuation control that can be achieved by applying such a concept to the<br />

buried septum in a two-degree-of-freedom (2DOF) acoustic liner. An additional objective was to examine the adequacy of the<br />

existing impedance models to explain the behavior of the unique orifice shapes that result from the proposed silding perforate<br />

concept. Different orifice shapes with equivalent area were also examined to determine if highly non-circular orifices had a significant<br />

impact on the impedance.<br />

Derived from text<br />

Active Control; Orifices; Geometry; Acoustic Impedance; Linings; Resonance<br />

72<br />

ATOMIC AND MOLECULAR PHYSICS<br />

�������� ������ ��� ��������� ���������� �������� ����������� ��� ������ ��� ��������� �������� ��� ������������������ ������� ���<br />

�� ������� ��������<br />

<strong>2000</strong>0062712 Gesellschaft fuer Schwerionenforschung m.b.H., Darmstadt, Germany<br />

Examination of the e(sup +) <strong>and</strong> e(sup +)e(sup -) pair emission from heavy ion collisions at the EPoS II spectrometer<br />

Baumann, J.; Dec. 31, 1996; 150p; In German; In English<br />

Report No.(s): DE99-715815; GSI-96-05; No Copyright; Avail: Department of Energy Information Bridge<br />

In the course of examination of the positron <strong>and</strong> positron-electron pair emission from heavy ion collisions at the Coulomb<br />

barrier, the research groups EPOS I <strong>and</strong> ORANGE have found a number of line structures in the measured positron energy <strong>and</strong><br />

cumulative pair energy spectra which up to present could not be fully explained, as theoretical interpretations so far remain incon-<br />

191

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