LEADER 01968oam  2200577I  450 
001 9910713646103321
005 20200630130639.0
035   $a(CKB)5470000002503213
035   $a(OCoLC)1104148274
035   $a(EXLCZ)995470000002503213
100   $a20190610d1934      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic effects of a split flap on the spinning characteristics of a monoplane model /$fby M.J. Bamber
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1934.
215   $a1 online resource (8 pages, 5 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 515
300   $a"December 1934"
300   $aNo Federal Depository Library Program (FDLP) item number
320   $aIncludes bibliographical references (page 8)
606   $aAerodynamics
606   $aSpin (Aerodynamics)
606   $aSplit flaps (Airplanes)
606   $aWind tunnel testing
606   $aAerodynamics$2fast
606   $aSpin (Aerodynamics)$2fast
606   $aSplit flaps (Airplanes)$2fast
606   $aWind tunnel testing$2fast
615  0$aAerodynamics.
615  0$aSpin (Aerodynamics)
615  0$aSplit flaps (Airplanes)
615  0$aWind tunnel testing.
615  7$aAerodynamics.
615  7$aSpin (Aerodynamics)
615  7$aSplit flaps (Airplanes)
615  7$aWind tunnel testing.
700   $aBamber$b M. J.$01386953
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bTRAAL
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910713646103321
996   $aAerodynamic effects of a split flap on the spinning characteristics of a monoplane model$93450762
997   $aUNINA