LEADER 01796oam  2200517   450 
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005 20220210083912.0
035   $a(CKB)5470000002528545
035   $a(OCoLC)1154792555
035   $a(EXLCZ)995470000002528545
100   $a20200519d1939      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA method of estimating the critical buckling load for structural members /$fby Eugene E. Lundquist
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1939.
215   $a1 online resource (25 pages, 11 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 717
300   $a"July 1939."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 25).
606   $aStructural design
606   $aBuckling (Mechanics)
606   $aMathematical analysis
606   $aBuckling (Mechanics)$2fast
606   $aMathematical analysis$2fast
606   $aStructural design$2fast
615  0$aStructural design.
615  0$aBuckling (Mechanics)
615  0$aMathematical analysis.
615  7$aBuckling (Mechanics)
615  7$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   $a9910717167003321
996   $aA method of estimating the critical buckling load for structural members$93475833
997   $aUNINA