LEADER 01918oam  2200553   450 
001 9910717160003321
005 20220210084613.0
035   $a(CKB)5470000002528615
035   $a(OCoLC)1156323832
035   $a(EXLCZ)995470000002528615
100   $a20200602d1939      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPressure-distribution investigation of an N.A.C.A. 0009 airfoil with a 50-percent-chord plain flap and three tabs /$fby William G. Street and Milton B. Ames, Jr
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1939.
215   $a1 online resource (11 pages, 31 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 734
300   $a"November 1939."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 11).
606   $aAerofoils
606   $aAerodynamic load
606   $aFlaps (Airplanes)
606   $aAerodynamic load$2fast
606   $aAerofoils$2fast
606   $aFlaps (Airplanes)$2fast
615  0$aAerofoils.
615  0$aAerodynamic load.
615  0$aFlaps (Airplanes)
615  7$aAerodynamic load.
615  7$aAerofoils.
615  7$aFlaps (Airplanes)
700   $aStreet$b William G.$01418271
702   $aAmes$b Milton B.$cJr.,
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bOCLCF
801  2$bXFF
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910717160003321
996   $aPressure-distribution investigation of an N.A.C.A. 0009 airfoil with a 50-percent-chord plain flap and three tabs$93529204
997   $aUNINA