LEADER 01899oam  2200553   450 
001 9910716018403321
005 20210601132009.0
035   $a(CKB)5470000002517924
035   $a(OCoLC)20650453$z(OCoLC)761230175
035   $a(EXLCZ)995470000002517924
100   $a19891115j197301    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSummary of design and blade-element performance data for 12 axial-flow pump rotor configurations /$fby Max J. Miller [and four others]
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration,$dJanuary 1973.
215   $a1 online resource (iii, 214 pages) $cillustrations
225 1 $aNASA/TN ;$vD-7074
300   $a"January 1973."
320   $aIncludes bibliographical references (pages 213-214).
606   $aRotors$2nasat
606   $aBlades$2nasat
606   $aAxial flow$2nasat
606   $aPumping machinery$xDynamics$xComputer simulation
606   $aBlades$xDesign and construction$2fast
606   $aRotors$xDesign and construction$2fast
615  7$aRotors.
615  7$aBlades.
615  7$aAxial flow.
615  0$aPumping machinery$xDynamics$xComputer simulation.
615  7$aBlades$xDesign and construction.
615  7$aRotors$xDesign and construction.
700   $aMiller$b Max J$c(Of Lewis Research Center),$065049
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bABC
801  1$bABC
801  2$bAD#
801  2$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910716018403321
996   $aSummary of design and blade-element performance data for 12 axial-flow pump rotor configurations$93478317
997   $aUNINA