[1] 王永虎. 直升机飞行原理[M].成都:西南交通大学出版社, 2017.
WANG Yonghu. Principles of Helicopter Flight [M]. Chengdu: Southwest Jiaotong University Press, 2017.
[2] FLIGHT SAFETY FOUNDATION. FAA proposes new rules on cargo compartment fire detection and suppression[J]. Cabin Crew Safety, 1996, 31(6):1-12.
[3] LEWIS R B I. Army helicopter performance trends[J]. Journal of the American Helicopter Society, 1971, 17(2):15-23.
[4] JOHNSTON J F, COOK J R. AH-56A vehicle development[C]∥Proceedings of the American Helicopter Society 27th Annual Forum, Washington D. C., 1971: 1-10.
[5] ELLIN A D S. An inflight investigation of LYNX AH MK5 main rotor/tail rotor interactions[C]∥19th European Rotorcraft Forum. Italian Association of Aeronautics and Astronautics, Cemobbio, 1993.
[6] WIESNER W, KOHLER G. Tail rotor performance in presence of main rotor, ground, and winds[J]. Journal of the American Helicopter Society, 1973, 19(3):2-9.
[7] WIESNER W, KOHLER G. Tail Rotor Design Guide[R]. Springfield: National Technical Information Service, 1974, 50(12):102-102.
[8] WILLIAM J W. Advisory Circular 90-95 Unanticipated Right Yaw in Helicopters[S]. Washington D.C.: Federal Aviation Administration, 1995.
[9] PROUTY R W. Helicopter Performance, Stability, and Control[M].
Melbourne: Krieger Pub, 1995.
[10] SRINIVAS V, CHOPRA I, HAAS D, et al. Prediction of yaw control effectiveness and tail rotor loads[C]∥19th European Rotorcraft Forum. Italian Association of Aeronautics and Astronautics, Cemobbio, 1993.
[11] PROUTY R W. Development of the Empennage Configuration of the YAH-64 Advanced Attack Helicopter[R]. U.S.A.: US Army Aviation Research and Development Command, 1983.
[12] BLAKE B B, HODDER D S J, HANKER E J. Wind Tunnel Investiga-tion into the Directional Control Characteristics of an OH-58A Helicopter[M]. U.S.A.: US Army Aviation Research and Development Com-mand, 1984.
[13] KAYNES I W, PREATONI G, VISINGARDI A, et al. Heliflow pitch-up and quartering flight experiments[C]∥ 26th European Rotorcraft Forum. Hague, Netherlands, 2000.
[14] FLETCHER T M, BROWN R E. Helicopter tail rotor thrust and main rotor wake coupling in crosswind flight[J]. Journal of Aircraft, 2010, 47(6):2136-2148.
[15] Civil Aviation Department. Report on the Accident to Robinson R22 Helicopter[R]. Hong Kong: Accident Investigation Division, 2010.
[16] SEDDON J M, NEWMAN S. Basic Helicopter Aerodynamics[M]. New Jersey: John Wiley & Sons, 2011.
[17] Accident and Incident Investigation Division.Aircraft Accident Investiga-tion Report, Reference: CA18/2/3/9699[R]. South Africa: Civil Aviation Authority,2018.
[18] Office of Aviation Safety. Aviation Accident Summary CEN15FA003[R]. Washington D.C.: National Transportation Safety Board,2015.
[19] Office of Aviation Safety.Aviation Accident Summary CEN13TA165[R]. Washington D.C.: National Transportation Safety Board,2013.
[20] Office of Aviation Safety. Specialists Factual Report, ERA12MA005[R]. Washington D.C.: National Transportation Safety Board,2011.
[21] JAMES M T. Type B Accident Investigation Report of the April 23, 1997, Helicopter Accident at Raton Pass [R]. U.S.A.: Western Area Power Administration,1997. |