[1]J.Seddon, E.L.Goldsmith..Intake aerodynamics[M]. .AIAA EDUCATION SERIES, 1999, :-[2]Saeed Farokhi .Aircraft propulsion[M]..John Wiley & Sons Inc, 2008, :-[3]Yoram Yadlin, Arvin Shmilovich.Computational method for assessment of flow control Techniques for airplane propulsion systems[R]..AIAA 2008-4084, 2008, :-[4]CAO G Z, JI H H, HU Y P, et al.An icing model for simulating three dimensional ice accretion on the upwind surfaces of a plane[J].Journal of Aerospace Power, 2011, 26(9):1954-1963[5]曹广州,吉洪湖,胡娅萍等.模拟飞机迎风面三维积冰的数学模型[J].航空动力学报, 2011, 26(9):1954-1963[6]J.S.Sokhey.Analysis Of installed wind tunnel test results on large bypass ratio engine/nacelle installations[R].AIAA90-2146, 1990, :-[7]M.I.K.MacKinnon, B.K.Mehta.Factors influencing nacelle design on 747[R]..AIAA79-1236, 1979, :-[8]Kamel M. A., Theo G. K. J., Kenneth J. D. W..Icing calculations on a typical commercial jet engine inlet nacelle[R]. .AIAA94-0610, 1994, :-[9]Wonjin Jin, Ray Taghavi.Computational study of the effects of ice accretions on the flowfields in the M2129 S-Duct inlet[R]. .AIAA2008-75, 2008, :-[10]LI Y L, SHI X P.Investigation of the present status of research on bird impacting on commercial airplanes[J].Acta Aeronautica et Astronautica Sinica, 2012, 33(2):189-198[11]李玉龙,石霄鹏.民用飞机鸟撞研究现状[J].航空学报, 2012, 33(2):189-198[12]Wilbeck J.S.,Barber J[J].Bird impact loading. The shock and vibration bulletin, 1978, 48(2):115-122[13]Georgiadis S.Gunnion AJ.,Thomason R. S.,et al. Bird strike simulation for certification of the Boeing 787 composite moveable trailing edge[J].Composite structures, 2008, 86(1-3):258-268[14]Lavoie M.A.,Gakwaya A,Ensan M. N.,et al. Bird’s substitute tests results and evaluation of available numerical methods[J].International journal of impact engineering, 2009, 36(10-11):1276-1287[15]Stefan Kennedy, Theresa Robinson, Stephen Spence, et al.The effect of lipskin damage on inlet distortion[R].AIAA2010-747, 2010, :-[16]McCARTHY M A, Xiao J R, Petrinic N, et al.Modeling of bird strike on an aircraft wing leading edge made from fibre metal laminates-Part 1: Material modeling[J][J].Applied Composite Materials, 2004, 0(11):295-315[17]Hirose N, Asai K, Ikawa K.Transonic 3D Euler analysis of flows around fan-jet engine and T.P.S. (turbine powered simulator)[R]. NAL-TR-1045, 1989.[18]Richard J.RE. An investigation of several NACA 1-series axisymmetric inlets at mach numbers from 0.4 to 1.29[R]. NASA TM X-2917, 1974. |