1 Roskam J. Airplane Design. DAR Corporation, 1985
2 Thibert JJ, Reneaux J, Schmitt V.ONERA activities on drag reduction. The 14th Congress of ICAS, 1990
3 Joslin RD.Aircraft laminar flow control. Annual Review of Fluid Mechanics, 1998, 30(1): 1-29
4 Arcara PC, Bartlett DW, Mccullers LA.Analysis for the application of hybrid laminar flow control to a long-range subsonic transport aircraft. SAE Technical Paper, 1991
5 Joslin RD.Overview of laminar flow control. NASA/TP-1998-208705, 1998
6 Kachanov YS.Physical mechanisms of laminar-boundary-layer transition. Annual Review of Fluid Mechanics, 1994, 26(1): 411-482
7 Saric WS, Reed HL, White EB.Stability and transition of three-dimensional boundary layers. Annual Review of Fluid Mechanics, 2003, 35(1): 413-440
8 Saric WS.Görtler vortices. Annual Review of Fluid Mechanics, 1994, 26(1): 379-409
9 Herbert T.Secondary instability of boundary layers. Annual Review of Fluid Mechanics, 1988, 20(1): 487-526
10 Abbott IH, von Doenhoff AE. Theory of Wing Sections. Dover: Dover Publications Inc, 1959
11 Selig MS, Maughmer MD, Somers DM.Natural-laminar-flow airfoil for general-aviation applications.Journal of Aircraft, 1995, 32(4): 710-715
12 Dagenhart J, Saric WS.Cross-flow stability and transition experiments in swept-wing flow. NASA/TP-1999-209344, 1999
13 Crouch JD. Modeling transition physics for laminar flow control. AIAA Paper, 2008-3832, 2008
14 Fischer MC, Wright Jr AS, Wagner RD.A flight test of laminar flow control leading-edge systems. NASA-TM-85712, 1983
15 Powell AG.The right wing of the LEFT airplane. NASA, Langley Research Center, Research in Natural Laminar Flow and Laminar-Flow Control, N90-12503, 1987
16 Lange RH.Lockheed laminar-flow control systems development and applications. NASA, Langley Research Center, Research in Natural Laminar Flow and Laminar-Flow Control, N90-12506, 1987
17 Collier Jr FS.An overview of recent subsonic laminar flow control flight experiments. AIAA, 24th Fluid Dynamics Conference, Orlando, FL, 1993
18 William S, Ruben Jr B.Leading-edge roughness as a transition control Mechanism. 36th AIAA Aerospace Sciences Meeting and Exhibit, 1998
19 19 Carpenter AL, Saric WS, Reed HL. In-flight receptivity experiments on a 30-degree swept-wing using micron-sized discrete roughness elements. [PhD Thesis]. Texas: Texas A & M University, 2010
20 Fransson JHM, Talamelli A, Brandt L, et al.Delaying transition to turbulence by a passive mechanism. Physical Review Letters, 2006, 96(6): 064501
21 Cossu C, Brandt L.On Tollmien-Schlichting-like waves in streaky boundary layers. European Journal of Mechanics-B/Fluids, 2004, 23(6): 815-833
22 Shahinfar S, Sattarzadeh SS, Fransson JHM, et al.Revival of classical vortex generators now for transition delay. Physical Review Letters, 2012, 109(7): 074501
23 Sattarzadeh SS, Fransson JHM, Talamelli A, et al.Consecutive turbulence transition delay with reinforced passive control. Physical Review E, 2014, 89(6): 061001
24 Barckmann K, Tropea C, Grundmann S.Attenuation of Tollmien-Schlichting waves using plasma actuator vortex generators. AIAA Journal, 2015, 53(5): 1384-1388
25 Kramer MO.Boundary-layer stabilization by distributed damping. J Aeronautical Sciences, 1957, 24: 459-460
26 Kramer MO.Boundary-layer stabilization by distributed damping. J American Society of Naval Engineers, 1960, 72: 25-33
27 Gaster M.Is the dolphin a red herring? //Liepmann HW, Narasimha R, eds. IUTAM Symp on Turbulence Management and Relaminarisation. Berlin, Heidelberg, New York: Springer, 1987
28 Carpenter PW, Lucey AD, Davies C.Progress on the use of compliant walls for laminar-flow control. Journal of Aircraft, 2001, 38(3): 504-512
29 Robinson SK.Coherent motions in the turbulent boundary layer. Annual Review of Fluid Mechanics, 1991, 23(1): 601-639
30 Kline SJ, Robinson SK.Quasi-coherent structures in the turbulent boundary layer. I—Status report on a community-wide summary of the data//Near-Wall Turbulence. New York: Hemisphere Phblishing Corp, 1990
31 Dean B, Bhushan B.Shark-skin surfaces for fluid-drag reduction in turbulent flow: a review. Philosophical Transactions of the Royal Society of London A: Mathematical, Physical and Engineering Sciences, 2010, 368(1929): 4775-4806
32 Walsh MJ.Turbulent boundary layer drag reduction using riblets. AIAA, 20th Aerospace Sciences Meeting, Orlando, FL, 1982
33 Suzuki Y, Kasagi N.Turbulent drag reduction mechanism above a riblet surface. AIAA Journal, 1994, 32(9): 1781-1790
34 Viswanath PR.Aircraft viscous drag reduction using riblets. Progress in Aerospace Sciences, 2002, 38(6): 571-600
35 Mclean J, George-Falvy D, Sullivan P.Flight-test of turbulent skin-friction reduction by riblets. Turbulent Drag Reduction by Passive Means, Royal Aeronautical Society, 1987
36 Walsh MJ, Anders JB.Riblet/LEBU research at NASA Langley. Applied Scientific Research, 1989, 46(3): 255-262
37 Szodruch J. Viscous drag reduction on transport aircraft. AIAA paper, 1991-0685, 1991
38 Mcginleyt CB.Riblet drag reduction at plight conditions. AIAA, 6th Applied Aerodynamics Conference, Williamsburg, 1988
39 Karniadakis GE, Choi KS.Mechanisms on transverse motions in turbulent wall flows. Annual Review of Fluid Mechanics, 2003, 35: 45-62
40 Choi KS, Debisschop JR, Clayton BR.Turbulent boundary-layer control by means of spanwise-wall oscillation. AIAA Journal, 1998, 36(7): 1157-1163
41 Kim K, Sung HJ.Effects of unsteady blowing through a spanwise slot on a turbulent boundary layer. Journal of Fluid Mechanics, 2006, 557: 423-450
42 Tardu SF.Active control of near-wall turbulence by local oscillating blowing. Journal of Fluid Mechanics, 2001, 439: 217-253
43 Whalley RD, Choi KS.The starting vortex in quiescent air induced by dielectric barrier discharge plasma. Journal of Fluid Mechanics, 2012, 703: 192-203
44 Jukes TN, Choi KS, Johnson GA, et al.Turbulent drag reduction by surface plasma through spanwise flow oscillation. The 3rd AIAA Flow Control Conference, 2006
45 45 Jukes TN. Turbulent drag reduction using surface plasma. [PhD Thesis]. Nottingham, UK: University of Nottingham, 2007
46 Whalley RD, Choi KS.Turbulent boundary-layer control with spanwise travelling waves. Journal of Physics, 2011, 318(2): 022039
47 Wang JJ, Choi KS, Feng LH, et al.Recent developments in DBD plasma flow Control. Progress in Aerospace Sciences, 2013, 62: 52-78
48 Whalley RD, Choi KS.Turbulent boundary-layer control with span-wise travelling waves. Journal of Physics, 2011, 318(2): 022039
49 Whitcomb RT.A design approach and selected wind tunnel results at high subsonic speeds for wing-tip mounted winglets. NASA-TN-D8260, 1976
50 Mattos B, Macedo A, Silva FD.Considerations about winglet Design. 21st AIAA Applied Aerodynamics Conference, 2003
51 Montoya LC.KC-135 winglet flight results. https://ntrs. nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19810010485. pdf
52 Bourdin P, Gatto A, Friswell MI.Aircraft control via variable cant-angle Winglets. Journal of Aircraft, 2008, 45(2): 414-423
53 刘沛清著. 流体力学通论. 北京:科学出版社,2017
54 Whitcomb RT.A study of the zero-lift drag-rise characteristics of wing-body combinations near the speed of sound. NACA-TR-1273, 1952
55 Whitcomb RT, Fiscetti TL.Development of a supersonic area rule and an application to the design of a wing-body combination having high lift-to-drag ratios. NACA RM L53B31a, 1953
56 Tai T, Huson G, Hicks R, et al.Transonic characteristics of a humped airfoil. Journal of Aircraft, 1988, 25(8): 673-674
57 Milholen WE, Owens LR. On the application of contour bumps for transonic drag reduction. AIAA paper, 2005-0462, 2005
58 Stanewsky E, Délery J, Fulker J, et al.Synopsis of the Project EUROSHOCK II. Drag Reduction by Shock and Boundary Layer Control. Berlin, Heidelberg: Springer, 2002
59 McGowan AMR. AVST morphing project research summaries in fiscal year 2001. NASA/TM-2002-211769, 2002
60 Bruce PJK, Colliss SP.Review of research into shock control bumps. Shock Waves, 2015, 25(5): 451-471
61 Eastwood JP, Jarrett JP.Toward designing with three-dimensional bumps for lift/drag improvement and buffet alleviation. AIAA Journal, 2012, 50(12): 2882-2898