- Abstract
- Introduction
- Computational Aeroelastic Analysis
- Results and Discussion
- Conclusion

http://chineseinput.net/에서 pinyin(병음)방식으로 중국어를 변환할 수 있습니다.
변환된 중국어를 복사하여 사용하시면 됩니다.
https://www.riss.kr/link?id=A76340915
2003
English
SCIE,SCOPUS,KCI등재
학술저널
34-44(11쪽)
0
상세조회0
다운로드목차 (Table of Contents)
Reconfigurable Flight Control System Design Using Sliding Mode Based Model Following Control Scheme
A Study on Assessment of Composite Couplings for Helicopter Rotor Blades with Multi-cell Sections
Wind Tunnel Test of the Straight and Forward Swept Canards
Recess Effects on Spray Characteristics of Swirl Coaxial Injectors