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https://www.riss.kr/link?id=O46971661
2006년
eng
1068-7998
SCOPUS
학술저널
RUSSIAN AERONAUTICS C/C OF IZVESTIIA VYSSHIE UCHEBNYE ZAVEDENIIA AVIATSIONNAIA TEKHNIKA
80-85 [※수록면이 p5 이하이면, Review, Columns, Editor's Note, Abstract 등일 경우가 있습니다.]
0
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A technique for designing highly-stiffened chevron folded cores
Thermohyperelasticity model and its application to the study of inflated plate instability. II
Parametrization method for the median surface of a thin-walled structure element
Results of experimental studies of gyroplane main rotor hub loads under unsteady flight conditions