魏志强,徐肖豪.飞机尾涡流场的建模与仿真计算研究[J].交通运输系统工程与信息,2010,10(4):186-191. WEI Zhi-qiang, XU Xiao-hao. Modeling and simulating of flow field for aircraft wake vortex[J]. Journal of Transportation Systems Engineering and Information Technology, 2010, 10(4): 186-191.(in Chinese)
[2]
VICROY D D, VIJGEN P M, REIMER H M, et al. Recent NASA wake-vortex flight tests, flow-physics database and wake-development analysis[C]∥AIAA. World Aviation Congress and Exposition. Anaheim: AIAA, 1998: 1-14.
[3]
LIOT D. Wake vortex encounter model implementation and validation in the online(piloted)flight simulation environment[R]. Toulouse: WAVENC Technical Note TN-19, AM Airbus, 2000.
[4]
DE BRUIN A C, SPEIJKER L J P, MOET H, et al. S-wake: assessment of wake vortex safety[R]. Amsterdam: National Aerospace Laboratory NLR, 2003.
[5]
LUCKNER R, H？HNE G, FUHRMANN M. Hazard criteria for wake vortex encounters during approach[J]. Aerospace Science and Technology, 2004, 8(8): 673-687.
[6]
BRANDON J M, JORDAN F L, STUEVER R A, et al. Application of wind tunnel free-flight technique for wake vortex encounters[R]. Washington DC: NASA, 1997.
[7]
PADFIELD G D, MANIMALA B, TURNER G P. A severity analysis for rotorcraft encounters with vortex wakes[J]. Journal of the American Helicopter Society, 2004, 49(4): 445-456.
[8]
LAWRENCE B, PADFIELD G D. Wake vortex encounter severity for rotorcraft in approach and landing[R]. Florence: 31st European Rotorcraft Forum, 2005.
[9]
胡 军,徐肖豪.空中交通中尾流间隔的研究[J].中国民航学院学报,2002,20(4):1-5. HU Jun, XU Xiao-hao. Wake vortex separation of ATC[J]. Journal of Civil Aviation University of China, 2002, 20(4): 1-5.(in Chinese)
[10]
冯志勇.尾流对飞行的影响及安全间隔研究[D].成都:西南交通大学,2007. FENG Zhi-yong. How wake vortexes affect the flights and safety separation research[D]. Chengdu: Southwest Jiaotong University, 2007.(in Chinese)
[11]
徐肖豪,赵鸿盛,杨传森,等.飞行进近中尾流的大涡数值模拟[J].南京航空航天大学学报,2010,42(2):179-184. XU Xiao-hao, ZHAO Hong-sheng, YANG Chuan-sen, et al. Large eddy simulation of wake vortex during approach[J]. Journal of Nanjing University of Aeronautics and Astronautics, 2010, 42(2): 179-184.(in Chinese)
[12]
徐肖豪,赵鸿盛,王振宇.尾流间隔缩减技术综述[J].航空学报,2010,31(4):655-662. XU Xiao-hao, ZHAO Hong-sheng, WANG Zhen-yu. Overview of wake vortex separation reduction systems[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(4): 655-662.(in Chinese)
[13]
POIREL D, PRICE S J. Bifurcation characteristics of a two-dimensional structurally non-linear airfoil in turbulent flow[J]. Nonlinear Dynamics, 2007, 48(4): 423-435.
[14]
BROWN A. The impact upon aircraft airworthiness design from encounters with discrete vortices[C]∥AIAA. 44th AIAA Aerospace Sciences Meeting and Exhibit. Reno: AIAA, 2006: 1-19.
[15]
CROW S C. Stability theory for a pair of trailing vortices[J]. AIAA Journal, 1970, 8(12): 2172-2179.
