LEADER 02235oam  2200625   450 
001 9910716990503321
005 20211026141217.0
035   $a(CKB)5470000002526287
035   $a(OCoLC)1154792930
035   $a(EXLCZ)995470000002526287
100   $a20200519d1939      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPressure-distribution measurements on a tapered wing with a full-span split flap in curved flight /$fby Th. Troller and F. Rokus
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1939.
215   $a1 online resource (8 pages, 8 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 683
300   $a"January 1939."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 8).
606   $aAirplanes$xWings
606   $aSplit flaps (Airplanes)
606   $aAerodynamic load$xMeasurement
606   $aRolling (Aerodynamics)
606   $aYawing (Aerodynamics)
606   $aAerodynamic load$xMeasurement$2fast
606   $aAirplanes$xWings$2fast
606   $aRolling (Aerodynamics)$2fast
606   $aSplit flaps (Airplanes)$2fast
606   $aYawing (Aerodynamics)$2fast
615  0$aAirplanes$xWings.
615  0$aSplit flaps (Airplanes)
615  0$aAerodynamic load$xMeasurement.
615  0$aRolling (Aerodynamics)
615  0$aYawing (Aerodynamics)
615  7$aAerodynamic load$xMeasurement.
615  7$aAirplanes$xWings.
615  7$aRolling (Aerodynamics)
615  7$aSplit flaps (Airplanes)
615  7$aYawing (Aerodynamics)
700   $aTroller$b T.$01414262
702   $aRokus$b Frank G.
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   $a9910716990503321
996   $aPressure-distribution measurements on a tapered wing with a full-span split flap in curved flight$93512978
997   $aUNINA