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035   $a(OCoLC)1107323650
035   $a(EXLCZ)995470000002498411
100   $a20190703d1921      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe effect of staggering a biplane /$fby F.H. Norton
210  1$a[Washington, D.C]. :$cNational Advisory Committee for Aeronautics,$d1921.
215   $a1 online resource (3 pages, 5 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 70
300   $a"September, 1921."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 1).
606   $aBiplanes
606   $aAirplanes$xWings$xDesign and construction
606   $aLift (Aerodynamics)
606   $aAirplanes$xWings$xDesign and construction$2fast
606   $aBiplanes$2fast
606   $aLift (Aerodynamics)$2fast
615  0$aBiplanes.
615  0$aAirplanes$xWings$xDesign and construction.
615  0$aLift (Aerodynamics)
615  7$aAirplanes$xWings$xDesign and construction.
615  7$aBiplanes.
615  7$aLift (Aerodynamics)
700   $aNorton$b F. H$g(Frederick Harwood),$f1896-1992,$018769
712 02$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   $a9910712977903321
996   $aThe effect of staggering a biplane$93461835
997   $aUNINA