지원사업
학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
커뮤니티
연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
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초록· 키워드
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The rotorcraft makes lift and control forces by the rotor thrust. At the development phase of the rotorcraft, the operational limitations have to be established. And it shall be demonstrated to operate the rotorcraft safely within the limitations. This paper introduces establishment and evaluation results of operational rotor speed limitations for the medium class utility rotorcraft. And it shows the follow-up activities after design changes of rotor speed indicators and aural warning systems for implementing the rotor speed limitations.
목차
등록된 정보가 없습니다.
참고문헌 (7)
참고문헌 신청
Alastair K. Cooke / 2002 / Helicopter Test and Evaluation / QinetiQ
Army Material Command / 1974 / Engineering Design Handbook. Helicopter Engineering. Part One.,Virginia
US. Federal Aviation Administration / 2011 / Federal Aviation Regulations Part 29 Airworthiness Standards : Transport Category rotorcraft
US. Headquarters Department of the Army / 1996 / Operator’s Manual for UH-60A, UH-60L, EH-60A Helicopter, TM 1-1520-237-10, Washington D.C
Eurocopter / 2006 / Flight Manual AS 532 U2, Marignane
Army Material Command / 1974 / Engineering Design Handbook. Helicopter Engineering. Part One.,Virginia
US. Federal Aviation Administration / 2011 / Federal Aviation Regulations Part 29 Airworthiness Standards : Transport Category rotorcraft
US. Headquarters Department of the Army / 1996 / Operator’s Manual for UH-60A, UH-60L, EH-60A Helicopter, TM 1-1520-237-10, Washington D.C
Eurocopter / 2006 / Flight Manual AS 532 U2, Marignane
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