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100   $a19910502j197302    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffect of a reduction in blade thickness on performance of a single-stage 20.32-centimeter mean-diameter turbine /$fby William J. Nusbaum and Milton G. Kofskey
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dFebruary 1973.
215   $a1 online resource (24 pages) $cillustrations
225 1 $aNASA/TN ;$vD-7128
300   $a"February 1973."
320   $aIncludes bibliographical references (page 11).
606   $aGas-turbines$xBlades
606   $aGas-turbines$xAerodynamics
606   $aGas-turbines$xAerodynamics$2fast
606   $aGas-turbines$xBlades$2fast
615  0$aGas-turbines$xBlades.
615  0$aGas-turbines$xAerodynamics.
615  7$aGas-turbines$xAerodynamics.
615  7$aGas-turbines$xBlades.
700   $aNusbaum$b William J.$01413835
702   $aKofskey$b Milton G.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLewis Research Center.
801  0$bABC
801  1$bABC
801  2$bAD#
801  2$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bCOP
801  2$bGPO
906   $aBOOK
912   $a9910716674503321
996   $aEffect of a reduction in blade thickness on performance of a single-stage 20.32-centimeter mean-diameter turbine$93538409
997   $aUNINA