00821nam a2200205 a 4500001001500000005001500015008004100030040001900071049003000090052001700120082001500137100004800152245011300200260005300313300003100366502009400397653006900491900002800560963002700588WDM199900052  20201104145828991112s1989    us a          000   eng    a011001c0110010 lWM272020lWM272021c2fDP02a629.11bY46a0 a629.112211 a염찬홍,g廉贊弘,d1957-0KAC20170599111a(An)assumed strain finite element model for composite shells undergoing large deflection/dby Chan Hong Yeom  aCollege Park, MD:bUniversity of Maryland,c1989  axiv, 159 p.:bill.;c28 cm1 aThesis(Ph.D.) --bGraduate School of the Univ. of Maryland:cAerospace Engineering,d1989  aSTRAINaFINITEaMODELaCOMPOSITEaSHELLSaUNDERGOINGaDEFLECTION10aYeom, Chan-Hong,d1957-  aAerospaceaEngineering