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100   $a20200519d1939      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aLoads imposed on intermediate frames of stiffened shells /$fby Paul Kuhn
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1939.
215   $a1 online resource (30 pages, 14 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 687
300   $a"February 1939."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (pages 29-30).
606   $aShells (Engineering)
606   $aStructural frames
606   $aLoads (Mechanics)
606   $aMathematical analysis
606   $aLoads (Mechanics)$2fast
606   $aMathematical analysis$2fast
606   $aShells (Engineering)$2fast
606   $aStructural frames$2fast
615  0$aShells (Engineering)
615  0$aStructural frames.
615  0$aLoads (Mechanics)
615  0$aMathematical analysis.
615  7$aLoads (Mechanics)
615  7$aMathematical analysis.
615  7$aShells (Engineering)
615  7$aStructural frames.
700   $aKuhn$b Paul$03498
712 02$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   $a9910716980503321
996   $aLoads imposed on intermediate frames of stiffened shells$93533244
997   $aUNINA