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100   $a20191113d1927      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA load factor formula /$fby Roy G. Miller
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1927.
215   $a1 online resource (8 pages, 1 unnumbered page) $cillustration
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 263
300   $a"August 1927."
300   $aNo Federal Depository Library Program (FDLP) item number.
606   $aLoad factor design
606   $aMathematics$vFormulae
606   $aAirplanes$xWeight
606   $aLift (Aerodynamics)
606   $aAirplanes$xWeight$2fast
606   $aLift (Aerodynamics)$2fast
606   $aLoad factor design$2fast
606   $aMathematics$2fast
608   $aMathematical formulae.$2fast
615  0$aLoad factor design.
615  0$aMathematics
615  0$aAirplanes$xWeight.
615  0$aLift (Aerodynamics)
615  7$aAirplanes$xWeight.
615  7$aLift (Aerodynamics)
615  7$aLoad factor design.
615  7$aMathematics.
700   $aMiller$b Roy G.$01413842
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bTRAAL
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910713674503321
996   $aA load factor formula$93511281
997   $aUNINA