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100   $a20200623d1937      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aStability of structural members under axial load /$fby Eugene E. Lundquist
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1937.
215   $a1 online resource (29 pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 617
300   $a"October 1937."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 22).
606   $aStructural design
606   $aAxial loads
606   $aMathematical analysis
606   $aAxial loads$2fast
606   $aMathematical analysis$2fast
606   $aStructural design$2fast
615  0$aStructural design.
615  0$aAxial loads.
615  0$aMathematical analysis.
615  7$aAxial loads.
615  7$aMathematical analysis.
615  7$aStructural design.
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   $a9910716726503321
996   $aStability of structural members under axial load$93454209
997   $aUNINA