항공기 구조 | Aircraft Structures & Others

Design and analysis of UAM aircraft (including static & dynamic, crashworthiness analysis)

UAM 항공기 설계, 분석 (하중 도출, 강도 해석, 동특성 분석, 내추락 분석)

Derivation of V-n diagram based on FAA Part 23

Structural analysis for full-scale airframe

Development of crashworthiness analysis method

Evaluation of structural safety for key components of UAV and AAM

무인항공기 기체와 AAM 항공기 핵심 부품에 대한 구조 안전성 평가

Structural analysis for UAV structures including static and buckling characteristics

Structural analysis for composite external cases of fuel cell system of AAM

Manufacturing and tests (SHM, impact, modal, tensile) for composite wing structure of AAM

Development of EMA actuator for flap control of GA aircraft & blade pitch control of AAM

GA급 항공기용 플랩 제어와 AAM용 블레이드 제어용 전기-기계식 구동기 개발 

Analysis of kinetic behavior of linear actuators based on a multi-body dynamics (MBD)

Finite element analysis for estimating 1) thermal and static behaviors, and 2) dynamic behaviors (modal analysis)

Fatigue analysis including life estimation for key components of linear actuators using S-N curves of materials 

Development of single aisle commercial midclass aircraft centerafter fuselage and elevator

중형 항공기 동체와 엘리베이터 구조 해석 

Finite Element Analysis of centerafter fuselage

Mechanical properties test of composite materials for Elevator

Structural optimization for composite structures 

복합재 구조에 대한 구조 최적화

Structural optimization of composite structures (e.g., tidal current blade) 

Development of optimization algorithms coupled with commercial software ABAQUS