LEADER 01845oam  2200517   450 
001 9910716036103321
005 20210521115528.0
035   $a(CKB)5470000002517746
035   $a(OCoLC)1150919530
035   $a(EXLCZ)995470000002517746
100   $a20200416d1935      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA deflection formula for single-span beams of constant section subjected to combined axial and transverse loads /$fby Walter E. Burke
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1935.
215   $a1 online resource (24 pages, 21 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 540
300   $a"September 1935."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 16).
606   $aAxial loads
606   $aAirplanes$xFuselage
606   $aAeronautics$xResearch
606   $aAeronautics$xResearch$2fast
606   $aAirplanes$xFuselage$2fast
606   $aAxial loads$2fast
615  0$aAxial loads.
615  0$aAirplanes$xFuselage.
615  0$aAeronautics$xResearch.
615  7$aAeronautics$xResearch.
615  7$aAirplanes$xFuselage.
615  7$aAxial loads.
700   $aBurke$b Walter E.$01399821
712 02$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   $a9910716036103321
996   $aA deflection formula for single-span beams of constant section subjected to combined axial and transverse loads$93465776
997   $aUNINA