LEADER 02064oam  2200577   450 
001 9910713082903321
005 20200316140507.0
035   $a(CKB)5470000002499371
035   $a(OCoLC)1107323816
035   $a(EXLCZ)995470000002499371
100   $a20190703d1921      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffects of varying the relative vertical position of wing and fuselage /$fby L. Prandtl
210  1$a[Washington, D.C.] :$cNational Advisory Committee for Aeronautics,$d1921.
215   $a1 online resource (4 pages, 6 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 75
300   $a"December, 1921."
300   $a"Extract from the First Report of the Go?ttingen Aerodynamic Laboratory, Chap. IV, Sec. 7, pp. 118-120"--Page 1.
300   $a"Translated by the National Advisory Committee for Aeronautics"--Page 2.
300   $aNo Federal Depository Library Program (FDLP) item number.
606   $aAirplanes$xWings
606   $aAirplanes$xFuselage
606   $aAerodynamics
606   $aMechanical efficiency
606   $aAerodynamics$2fast
606   $aAirplanes$xFuselage$2fast
606   $aAirplanes$xWings$2fast
606   $aMechanical efficiency$2fast
615  0$aAirplanes$xWings.
615  0$aAirplanes$xFuselage.
615  0$aAerodynamics.
615  0$aMechanical efficiency.
615  7$aAerodynamics.
615  7$aAirplanes$xFuselage.
615  7$aAirplanes$xWings.
615  7$aMechanical efficiency.
700   $aPrandtl$b Ludwig$f1875-1953,$03749
712 02$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   $a9910713082903321
996   $aEffects of varying the relative vertical position of wing and fuselage$93531293
997   $aUNINA