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200 10$aNoise transmission loss of a rectangular plate in an infinite baffle /$fLouis A. Roussos
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dMarch 1985.
215   $a1 online resource (33 pages) $cillustrations
225 1 $aNASA technical paper ;$v2398
300   $a"March 1985."
300   $aPrepared at Langley Research Center.
320   $aIncludes bibliographical references (pages 12-13).
606   $aTransmission loss$2nasat
606   $aAerodynamic noise$2nasat
606   $aNoise propagation$2nasat
606   $aRectangular panels$2nasat
606   $aIntegral equations$2nasat
606   $aPlates (Engineering)$xNoise$xMathematical models
606   $aComposite materials$xNoise$xMathematical models
606   $aSound$xTransmission$xMathematical models
606   $aSound pressure$xMathematical models
606   $aVibration$xMathematical models
606   $aSound pressure$xMathematical models$2fast
606   $aSound$xTransmission$xMathematical models$2fast
606   $aVibration$xMathematical models$2fast
615  7$aTransmission loss.
615  7$aAerodynamic noise.
615  7$aNoise propagation.
615  7$aRectangular panels.
615  7$aIntegral equations.
615  0$aPlates (Engineering)$xNoise$xMathematical models.
615  0$aComposite materials$xNoise$xMathematical models.
615  0$aSound$xTransmission$xMathematical models.
615  0$aSound pressure$xMathematical models.
615  0$aVibration$xMathematical models.
615  7$aSound pressure$xMathematical models.
615  7$aSound$xTransmission$xMathematical models.
615  7$aVibration$xMathematical models.
700   $aRoussos$b Louis A.$01412313
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
712 02$aLangley Research Center.
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