LEADER 01733oam  2200505   450 
001 9910717118903321
005 20220215124216.0
035   $a(CKB)5470000002529030
035   $a(OCoLC)1157237705
035   $a(EXLCZ)995470000002529030
100   $a20200608d1940      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aChart for critical compressive stress of flat rectangular plates /$fby H.N. Hill
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics ;$d1940.
215   $a1 online resource (14 pages, 2 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vno. 773
300   $a"August 1940."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (pages 14).
606   $aPlates (Engineering)
606   $aStrains and stresses
606   $aMaterials$xCompression testing
606   $aPlates (Engineering)$2fast
606   $aStrains and stresses$2fast
615  0$aPlates (Engineering)
615  0$aStrains and stresses.
615  0$aMaterials$xCompression testing.
615  7$aPlates (Engineering)
615  7$aStrains and stresses.
700   $aHill$b H. N.$01391511
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bTRAAL
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910717118903321
996   $aChart for critical compressive stress of flat rectangular plates$93445356
997   $aUNINA