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035   $a(CKB)5470000002385431
035   $a(OCoLC)639241509
035   $a(EXLCZ)995470000002385431
100   $a20100608d1987      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA method for calculating turbulent boundary layers and losses in the flow channels of turbomachines$b[electronic resource] /$fLawrence F. Schumann
210  1$a[Washington, D.C.] :$c[National Aeronautics and Space Administration],$d[1987]
215   $a1 online resource (17 unnumbered pages $cdigital, PDF file
225 1 $aNASA technical memorandum ;$v88928
225 1 $aUSAAVSCOM technical report ;$v86-C-36
300   $aTitle from title screen (viewed June 7, 2010).
320   $aIncludes bibliographical references (page 6).
410  0$aNASA technical memorandum ;$v88928.
410  0$aAVSCOM technical report ;$v86-C-36.
606   $aChannel flow$2nasat
606   $aDiffusion$2nasat
606   $aTurbomachinery$2nasat
606   $aTurbulent boundary layer$2nasat
606   $aTurbulent flow$2nasat
615  7$aChannel flow.
615  7$aDiffusion.
615  7$aTurbomachinery.
615  7$aTurbulent boundary layer.
615  7$aTurbulent flow.
700   $aSchumann$b Lawrence F$01391746
712 02$aUnited States.$bNational Aeronautics and Space Administration.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697148103321
996   $aA method for calculating turbulent boundary layers and losses in the flow channels of turbomachines$93445770
997   $aUNINA