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035   $a(CKB)5470000002517762
035   $a(OCoLC)1150919534
035   $a(EXLCZ)995470000002517762
100   $a20200416d1935      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 13$aAn application of the von Ka??rma?n-Millikan laminar boundary-layer theory and comparison with experiment /$fby Albert E. Von Doenhoff
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1935.
215   $a1 online resource (11 pages, 9 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 544
300   $a"October 1935."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 11).
606   $aLaminar boundary layer
606   $aLaminar flow
606   $aAerodynamics
606   $aAerodynamics$2fast
606   $aLaminar boundary layer$2fast
606   $aLaminar flow$2fast
615  0$aLaminar boundary layer.
615  0$aLaminar flow.
615  0$aAerodynamics.
615  7$aAerodynamics.
615  7$aLaminar boundary layer.
615  7$aLaminar flow.
700   $aVon Doenhoff$b Albert E.$01415457
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910716034503321
996   $aAn application of the von Ka??rma?n-Millikan laminar boundary-layer theory and comparison with experiment$93540122
997   $aUNINA