[1] FOLLEN G J,ROSARIO R D,WAHLS R,et al.NASA's fundamental aeronautics subsonic fixed wing project:generation n+3 technology portfolio:SAE Technical Paper 2011-01-2521[R].Warrendale:SAE,2011.
[2] GREITZER E M,BONNEFOY P A,BLANCO E D R,et al.N+3 aircraft concept designs and trade studies,final report:Volume 1:NASA/CR-2010-216794[R].Washington,D.C.:NASA,2010.
[3] POTSDAM M A,PAGE M A,LIEBECK R H.Blended wing body analysis and design:AIAA-97-2317[R].Reston:AIAA,1997.
[4] BOLSUNOVSKY A L,BUZOVERYA N P,GUREVICH B I,et al.Flying wing-problems and decisions[J].Aircraft Design,2001,4(4):193-219.
[5] QIN N,VAVALLE A,LE MOIGNE A,et al.Aerodynamic studies for blended wing body aircraft:AIAA 2002-5448[R].Reston:AIAA,2002.
[6] QIN N,VAVALLE A,LE MOIGNE A,et al.Aerodynamic considerations of blended wing body aircraft[J].Progress in Aerospace Sciences,2004,40(6):321-343.
[7] PEIGIN S,EPSTEIN B.Computational fluid dynamics driven optimization of blended wing body aircraft[J].AIAA Journal,2006,44(11):2736-2745.
[8] FROTA J,NICHOLLS K,WHURR J,et al.Final activity report 2005-2010[R].EU:New Aircraft Concepts Research,2010.
[9] VOS R,GEUSKENS F J J M M,HOOGREEF M F M.A new structural design concept for blended wing body cabins:AIAA-2012-1998[R].Reston:AIAA,2012.
[10] GRANZEIER W.New cabin design concept for blended wing body aircraft:AIAA-2002-5888[R].Reston:AIAA,2002.
[11] MUKHOPADHYAY V,SOBIESZCZANSKI-SOBIESKI J,KOSAKA I,et al.Analysis design and optimization of non-cylindrical fuselage for blended-wing-body(BWB) vehicle:AIAA-2002-5664[R].Reston:AIAA,2002.
[12] MUKHOPADHYAY V.Blended-Wing-Body(BWB) fuselage structural design for weight reduction:AIAA-2005-2349[R].Reston:AIAA,2005.
[13] RODRIGUEZ D L.A multidisciplinary optimization method for designing boundary layer ingestion inlets[D].Caligornia:Standford University,2001:157-194.
[14] DAGGETT D L,KAWAI R,FRIEDMAN D.Blended wing body systems studies:Boundary layer ingestion inlets with active flow control:NASA/CR-2003-212670[R].Washington,D.C.:NASA,2003.
[15] KO Y Y A.The multidisciplinary design optimization of a distributed propulsion blended-wing-body aircraft[D].Virginia:Virginia Polytechnic Institute and State University,2003:14-23.
[16] KAWAI R T,FRIEDMAN D M,SERRANO L.Blended wing body(BWB) boundary layer ingestion(BLI) inlet configuration and system studies:NACA/CR-2006-214534[R].Washington,D.C.:NASA,2006.
[17] PLAS A P,SARGEANT M A,MADANI V,et al.Performance of a boundary layer ingesting(BLI) propulsion system:AIAA-2007-0450[R].Reston:AIAA,2007.
[18] PITERA D M,DEHAAN M,BROWN D,et al.Blended wing body concept development with open rotor engine integration:NASA/CR-2011-217303[R].Washington,D.C.:NASA,2011.
[19] FERRAR A M,O'BRIEN W F.Progress in boundary layer ingesting embedded engine research:AIAA-2012-4283[R].Reston:AIAA,2012.
[20] WAN T,SONG B C.Aerodynamic performance study of a modern blended-wing-body aircraft under severe weather situations:AIAA-2012-1037[R].Reston:AIAA,2012.
[21] CARTER M B,VICROY D D,PATEL D.Blended-Wing-Body transonic aerodynamics:Summary of ground tests and sample results:AIAA-2009-0935[R].Reston:AIAA,2009.
[22] VICROY D D.Blended-Wing-Body low-speed flight dynamics:summary of ground tests and sample results:N20090007690[R].Reston:AIAA,2009.
[23] WAKAYAMA S.Multidisciplinary design optimization of the blended-wing-body:AIAA-1998-4938[R].Reston:AIAA,1998.
[24] SAEPHAN S.Determination of tailless aircraft tumbling and stability characteristics through computational fluid dynamics[D].California:University of California,Davis,2006:73-80.
[25] PEIGIN S,EPSTEIN B.CFD driven optimization of blended wing body aircraft:AIAA-2006-3457[R].Reston:AIAA,2006.
[26] LEIFSSON L T,MASON W H,SCHETZ J A,et al.Multidisciplinary design optimization of low-airframe-noise transport aircraft:AIAA-2006-0230[R].Reston:AIAA,2006.
[27] STAELENS Y D,BLACKWELDER R F,PAGE M A.Study of belly-flaps to enhance lift-and pitching moment coefficient of a BWB-airplane:AIAA-2007-4176[R].Reston:AIAA,2007.
[28] KUNTAWALA N B,HICKEN J E,ZINGG D W.Preliminary aerodynamic shape optimization of a blended-wing-body aircraft configuration:AIAA-2011-0642[R].Reston:AIAA,2011.
[29] ROYSDON P F,KHALID M.Blended-Wing-Body lateral-directional stability investigation using 6DOF simulation:AIAA-2011-1563[R].Reston:AIAA,2011.
[30] LYU Z.Aerodynamic shape optimization of a blended-wing-body aircraft:AIAA-2013-0283[R].Reston:AIAA,2013.
[31] WILDSCHEK A.Flight dynamics and control related challenges for design of a commercial blended wing body aircraft:AIAA-2014-0599[R].Reston:AIAA,2014.
[32] SIOURIS S,QIN N.Study of the effects of wing sweep on the aerodynamic performance of a blended wing body aircraft[J].Proceedings of the Institution of Mechanical Engineers Part G:Journal of Aerospace Engineering,2007,221(1):47-55.
[33] 蒋瑾.翼身融合布局飞机总体参数影响规律研究[R].北京:中国商飞北研中心与清华大学联合招收博士后研究报告,2015:14-16,43-52,78-90.JIANG J.Impact of aerodynamic configuration parameters on the aerodynamic performance of a blended-wing-body civil aircraft[R].Beijing:BASTRI & Tsinghua University,2015:14-16,43-52,78-90(in Chinese).
[34] LIEBECK R H.Blended wing body design challenges:AIAA-2003-2659[R].Reston:AIAA,2003.
[35] ANALYTICAL METHODS,INC.MGAERO:A Cartesian multigrid Euler code for flow around arbitrary configurations user's manual version 3.5[M].2010.
[36] ROE P L.Approximate Riemann solvers,parameter vectors,and difference schemes[J].Journal of Computational Physics,1981,43(2):357-372.
[37] YOON S,JAMESON A.A multigrid LU-SSOR scheme for approximate Newton iteration applied to the Euler equations:NASA-CR-179524[R].California:NASA,1986.
[38] MENTER F R.Two-equation eddy-viscosity turbulence models for engineering applications[J].AIAA Journal,1994,32(8):1598-1605.
[39] 杨爱明,翁培奋,乔志德.用多重网格方法计算旋翼跨声速无粘流场[J].空气动力学学报,2004,22(3):313-318.YANG A M,WENG P F,QIAO Z D.Euler solutions of transonic flow for a helicopter rotor in hover using multigrid method[J].Acta Aerodynamica Sinica,2004,22(3):313-318(in Chinese).
[40] REDEKER G.DLR-F4 wing body configuration:AGARD AR-303[R].Neuilly sur Seine:AGARD,1994.
[41] BRODERSEN O.Drag prediction of engine-airframe interference effects using unstructured Navier-Stokes calculations[J].Journal of Aircraft,2002,39(6):927-935.
[42] 2nd AIAA CFD drag prediction workshop website[EB/OL].(2003-06-21) [2015-09-20].http://aaac.larc.nasa.gov/tsab/cfdlarc/aiaa-dpw/Work-shop2/workshop2.html.
[43] BELTRAMO M N,TRAPP D L,KIMOTOB W,et al.Parametric study of transport aircraft systems cost and weight:NASA CR151970[R].California:NASA,1977. |