LEADER 01871oam 2200565 450 001 9910716869803321 005 20210922132024.0 035 $a(CKB)5470000002525486 035 $a(OCoLC)1159597667 035 $a(EXLCZ)995470000002525486 100 $a20200623d1938 ua 0 101 0 $aeng 135 $aurbn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aTables of stiffness and carry-over factor for structural members under axial load /$fby Eugene E. Lundquist and W.D. Kroll 210 1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1938. 215 $a1 online resource (22 pages) 225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 652 300 $a"June 1938." 300 $aNo Federal Depository Library Program (FDLP) item number. 320 $aIncludes bibliographical references (page 6). 606 $aStructural design 606 $aAxial loads 606 $aLoads (Mechanics) 606 $aMathematical models$vTables 606 $aAxial loads$2fast 606 $aLoads (Mechanics)$2fast 606 $aStructural design$2fast 615 0$aStructural design. 615 0$aAxial loads. 615 0$aLoads (Mechanics) 615 0$aMathematical models 615 7$aAxial loads. 615 7$aLoads (Mechanics) 615 7$aStructural design. 700 $aLundquist$b Eugene E.$01386894 702 $aKroll$b W. D. 712 02$aUnited States.$bNational Advisory Committee for Aeronautics, 801 0$bTRAAL 801 1$bTRAAL 801 2$bOCLCO 801 2$bTRAAL 801 2$bOCLCF 801 2$bGPO 906 $aBOOK 912 $a9910716869803321 996 $aTables of stiffness and carry-over factor for structural members under axial load$93521110 997 $aUNINA