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100   $a20151005d2000||||  u||            |
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135   $aur|n|---|||||
200 10$aEconomics of Medicare Reform$b[electronic resource]
210   $aKalamazoo $cW. E. Upjohn Institute for Employment Research$d2000
215   $a1 online resource (193 p.)
300   $aDescription based upon print version of record.
311   $a0-88099-212-3 
327   $a""Contents""; ""Acknowledgements""; ""The Authors""; ""1 - The Rise and FAll of Medicare""; ""2 - A Brief History of Social Insurance for the Aged in the United States""; ""3 - The Theory of Paying for Retirement""; ""4 - Forecasting Earnings""; ""5 - Estimating the Future Cost of Retirement Health Care Costs""; ""6 - Transition to Fully Funded Medicare""; ""7 - Conclusions and Other Issues in the Medicare Reform Debate""; ""Appendix A: Appendix to Chapter 3""; ""Appendix B: Appendix to Chapter 4""; ""References""; ""Author Index""; ""Subject Index""; ""About the Institute""
606   $aHealth care reform
606   $aMedicare -- Economic aspects
606   $aMedicare -- Finance
606   $aMedicare
608   $aElectronic books.
615  4$aHealth care reform.
615  4$aMedicare -- Economic aspects.
615  4$aMedicare -- Finance.
615  4$aMedicare.
676   $a338.4/33684/2600973
700   $aRettenmaier$b Andrew J$0977093
701   $aSaving$b Thomas R$0604011
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181   $ctxt$2rdacontent
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200 10$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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