LEADER 01692oam  2200493   450 
001 9910716999003321
005 20211022125344.0
035   $a(CKB)5470000002526201
035   $a(OCoLC)1154320596
035   $a(EXLCZ)995470000002526201
100   $a20200514d1938      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA method of rapidly estimating the position of the laminar separation point /$fby Albert E. von Doenhoff
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1938.
215   $a1 online resource (9 pages, 1 unnumbered page) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 671
300   $a"October 1938."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 9).
606   $aLaminar boundary layer
606   $aAerofoils
606   $aAerodynamic load
606   $aAerofoils$2fast
606   $aLaminar boundary layer$2fast
615  0$aLaminar boundary layer.
615  0$aAerofoils.
615  0$aAerodynamic load.
615  7$aAerofoils.
615  7$aLaminar boundary layer.
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   $a9910716999003321
996   $aA method of rapidly estimating the position of the laminar separation point$93517588
997   $aUNINA