부구조물 합성법을 이용한 접는 미사일 조종날개 모델 수립Model Establishment of a Deployable Missile Control Fin Using Substructure Synthesis Method

Publisher
한국소음진동공학회
Issue Date
2005-07
Language
KOR
Citation

한국소음진동공학회논문집, v.15, no.7, pp.813 - 820

metadata.dc.identifier.alternativecitation
Journal of The Korean Society for Noise and Vibratioin Engineering, v.15, no.7, pp.813-820
ISSN
1598-2785
URI
http://hdl.handle.net/10203/8493
Appears in Collection
AE-Journal Papers(저널논문)
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