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100   $a20200304d1933      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aComparison of three methods for calculating the compressive strength of flat and slightly curved sheet and stiffener combinations /$fby Eugene E. Lundquist
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1933.
215   $a1 online resource (19 pages, 12 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 455
300   $a"March, 1933."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 17).
606   $aAirplanes$xDesign and construction
606   $aMonocoque construction
606   $aPlates (Engineering)
606   $aStrength of materials
606   $aAirplanes$xDesign and construction$2fast
606   $aMonocoque construction$2fast
606   $aPlates (Engineering)$2fast
606   $aStrength of materials$2fast
615  0$aAirplanes$xDesign and construction.
615  0$aMonocoque construction.
615  0$aPlates (Engineering)
615  0$aStrength of materials.
615  7$aAirplanes$xDesign and construction.
615  7$aMonocoque construction.
615  7$aPlates (Engineering)
615  7$aStrength of materials.
700   $aLundquist$b Eugene E.$01386894
712 02$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   $a9910715228903321
996   $aComparison of three methods for calculating the compressive strength of flat and slightly curved sheet and stiffener combinations$93541385
997   $aUNINA