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동체의 유연성을 고려한 회전익 항공기 하중해석 프로그램 개발 : Development of Rotorcraft Trim Analysis Including Fuselage Component Flexibility

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Authors

곽진성

Advisor
신상준
Major
기계항공공학부
Issue Date
2011-02
Publisher
서울대학교 대학원
Keywords
헬리콥터기하학적 정밀 보유한 상태 동적 유입류동체 모델기동비행HelicopterGeometrically exact beamFinite state dynamic inflowFuselageManeuver
Description
학위논문 (석사)-- 서울대학교 대학원 : 기계항공공학부, 2011.2. 신상준.
Language
kor
URI
https://hdl.handle.net/10371/157393

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