LEADER 01788oam  2200493   450 
001 9910716021303321
005 20210528125959.0
035   $a(CKB)5470000002517895
035   $a(OCoLC)1150919730
035   $a(EXLCZ)995470000002517895
100   $a20200416d1936      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA method of estimating the aerodynamic effects of ordinary and split flaps of airfoils similar to the Clark Y /$fby H.A. Pearson
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1936.
215   $a1 online resource (19 pages, 12 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 571
300   $a"June 1936."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 18).
606   $aAerofoils
606   $aSplit flaps (Airplanes)
606   $aAerodynamics$xForecasting
606   $aAerofoils$2fast
606   $aSplit flaps (Airplanes)$2fast
615  0$aAerofoils.
615  0$aSplit flaps (Airplanes)
615  0$aAerodynamics$xForecasting.
615  7$aAerofoils.
615  7$aSplit flaps (Airplanes)
700   $aPearson$b Henry A$g(Henry Adolph),$f1906-$01398867
712 02$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   $a9910716021303321
996   $aA method of estimating the aerodynamic effects of ordinary and split flaps of airfoils similar to the Clark Y$93463074
997   $aUNINA