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035   $a(OCoLC)1159597651
035   $a(EXLCZ)995470000002525389
100   $a20200623d1938      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aInterference of wing and fuselage from tests of 18 combinations in the N.A.C.A. variable-density tunnel combinations with split flaps /$fby Albert Sherman
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1938.
215   $a1 online resource (9 pages, 7 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 640
300   $a"March, 1938."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 7).
606   $aAirplanes$xWings$xTesting
606   $aAirplanes$xFuselage$xTesting
606   $aSplit flaps (Airplanes)
606   $aInterference (Aerodynamics)
606   $aWind tunnel testing
606   $aAirplanes$xFuselage$xTesting$2fast
606   $aInterference (Aerodynamics)$2fast
606   $aSplit flaps (Airplanes)$2fast
606   $aWind tunnel testing$2fast
615  0$aAirplanes$xWings$xTesting.
615  0$aAirplanes$xFuselage$xTesting.
615  0$aSplit flaps (Airplanes)
615  0$aInterference (Aerodynamics)
615  0$aWind tunnel testing.
615  7$aAirplanes$xFuselage$xTesting.
615  7$aInterference (Aerodynamics)
615  7$aSplit flaps (Airplanes)
615  7$aWind tunnel testing.
700   $aSherman$b Albert$01386917
712 02$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   $a9910716879403321
996   $aInterference of wing and fuselage from tests of 18 combinations in the N.A.C.A. variable-density tunnel combinations with split flaps$93469467
997   $aUNINA