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035   $a(CKB)5470000002517682
035   $a(OCoLC)608110847
035   $a(EXLCZ)995470000002517682
100   $a20100420d1935      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aBending stresses due to torsion in cantilever box beams /$fby Paul Kuhn
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1935.
215   $a1 online resource (17 pages, 8 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 530
300   $a"June 1935."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 16).
606   $aAirplanes$xDesign and construction
606   $aStrains and stresses
606   $aAeronautics$xResearch
606   $aAeronautics$xResearch$2fast
606   $aAirplanes$xDesign and construction$2fast
606   $aStrains and stresses$2fast
615  0$aAirplanes$xDesign and construction.
615  0$aStrains and stresses.
615  0$aAeronautics$xResearch.
615  7$aAeronautics$xResearch.
615  7$aAirplanes$xDesign and construction.
615  7$aStrains and stresses.
700   $aKuhn$b Paul$03498
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bTRAAL
801  2$bGPO
906   $aBOOK
912   $a9910716042403321
996   $aBending stresses due to torsion in cantilever box beams$93498325
997   $aUNINA