학위논문
An assumed strain finite element model for composite shells undergoing large deflection
표제/저자사항 An assumed strain finite element model for composite shells undergoing large deflection / by Chan Hong Yeom
발행사항 College Park, MD: University of Maryland, 1989
형태사항 xiv, 159 p.: ill.; 28 cm
주기사항 Thesis(Ph.D.) -- Graduate School of the Univ. of Maryland: Aerospace Engineering, 1989
분류기호 듀이십진분류법-> 629.11
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