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Showing results 1 to 9 of 9

1
Aeroelastic Analysis of a Wing with Freeplay in the Subsonic/Transonic Regions

Yoo, Jae-Han; Park, Young-Keun; Lee, In; Han, Jae-Hung, 14th International Symposium in Advanced Fluid Information, pp.88-91, 2004-11

2
Frequency and time domain flutter computations of a wing with oscillating control surface including shock interference effects

Kwon, HJ; Kim, DH; Lee, In, AEROSPACE SCIENCE AND TECHNOLOGY, v.8, no.6, pp.519 - 532, 2004-09

3
Nonlinear aeroelastic simulation of a full-span aircraft with oscillating control surfaces

Yoo, JH; Kim, DH; Kwon, HJ; Lee, In, JOURNAL OF AEROSPACE ENGINEERING, v.18, no.3, pp.156 - 167, 2005-07

4
Numerical investigation on the aeroelastic instability of a complete aircraft model

Kim, JY; Kwon, HJ; Kim, KS; Lee, In; Han, Jae-Hung, JSME INTERNATIONAL JOURNAL SERIES B-FLUIDS AND THERMAL ENGINEERING , v.48, no.2, pp.212 - 217, 2005-05

5
구조 강성에 따른 교량 구조물의 임계 플러터 속도 연구

권혁준; 김종윤; 박성종; 이인; 한재흥, 한국전산구조공학회논문집, v.17, no.3, pp.271 - 278, 2004-09

6
구조 비선형성을 고려한 공탄성 특성 및 플러터 억제 = Aeroelastic characteristics and flutter suppression considering structural nonlinearitylink

배재성; Bae, Jae-Sung; et al, 한국과학기술원, 2002

7
다상연계 개념에 기초한 새로운 공탄성 해석 기법 개발 = The development of a new aeroelastic analysis method based on the multi-phase interaction perspectivelink

이승준; Lee, Seung-Jun; et al, 한국과학기술원, 2010

8
다중 구조 비선형성을 고려한 미사일 조종날개의 공탄성 해석 = Aeroelastic analysis of missile fin considering multiple structural nonlinearitieslink

서영진; Seo, Young-Jin; et al, 한국과학기술원, 2010

9
받음각 및 조종면 변위가 있는 날개의 천음속 공탄성 해석 = Transonic aeroelastic analysis of a wing with angle-of-attack and control surface deflectionlink

유재한; Yoo, Jae-Han; et al, 한국과학기술원, 2001

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