QIAO Z D, Airfoil selection and design, in: FANG B R, Aircraft aerodynamic layout design[M]. Aviation industry press, 1997 (in Chinese).

RAYMER D. Aircraft design: A conceptual approach[M]. 5th edition. Washington, DC: AIAA, Inc. , 2012. doi: 10.2514/4.869112

ANDERSON J D. Introduction to flight[M]. 8th edition. Boston: McGraw-Hill Book Company, 2008.

PADFIELD G D, LAWRENCE B. The birth of flight control: an engineering analysis of the wright brothers' 1902 glider[J]. Aeronautical Journal, 2003, 107(1078): 697-718.

HICKS R M, HENNE P A. Wing design by numerical optimization[J]. Journal of Aircraft, 1978, 15(7): 407-412. DOI:10.2514/3.58379

ACKROYD J A D. Sir George Cayley: The invention of the aeroplane near Scarborough at the time of Trafalgar[J]. Journal of Aeronautical History, 2011, 6: 130-181.https://www.aerosociety.com/media/4862/sir-george-cayley-the-invention-of-the-aeroplane-near-scarborough-at-the-time-of-trafalgar.pdf

BART G C. On aerial navigation[J]. The Journal of the Royal Aeronautical Society, 1955, 59(530): 110-119. DOI:10.1017/s0368393100130202

ANDERSON D Jr. Fundamentals of aerodynamics[M ] . 5 th edition. Aviation Industry Press, 2014 (in Chinese).

LILIENTHAL O. Bird flight as the basis of aviation : A Contribution Towards a System of Aviation[M ] . Longmans, Green and Company Limited, 1911. https://s3-eu-west-1.amazonaws.com/bga-sg-archive/Books/BIRDFLIGHT%20AS%20THE%20BASIS%20OF%20AVIATION.pdf

LI C Z. The development of aeroplane wings[C]//China Academic Journal Electronic Publishing House, 1998 (in Chinese).

ELLIOT B A. Herald of an age[M]. Arcadia Publishing, 2000.

AERONAUTICS N. Annual report of the national advisory committee for aeronautics (1st)[R]. Technical Report Archive Image Library, 1916.

BOBBITT P J. Langley airfoil-research program[R ] . NASA, N79-20032, 1979. https://ntrs.nasa.gov/api/citations/19790011861/downloads/19790011861.pdf

NICHELSON B J. Engineer in charge: a history of the langley aeronautical laboratory, 1917-1958. James R. Hansen[J]. Isis, 1988, 79(2): 319-320. DOI:10.1086/354738

JACOBS E N, WARD K E, PINKERTON R M. The characteristics of 78 related airfoil sections from tests in the variable-density wind tunnel[R ] . NACA-TR-460, 1933. https://ntrs.nasa.gov/api/citations/19930091108/downloads/19930091108.pdf

JACOBS E N, PINKERTON R M. Tests in the variable-density wind tunnel of related airfoils having the maximum camber unusually far forward[R ] . NACA-TR-537, 1936. https://ntrs.nasa.gov/api/citations/19930091610/downloads/19930091610.pdf

JACOBS E N, PINKERTON R M, GREENBERG H. Tests of related forward-camber airfoils in the variable-density wind tunnel[R ] . NACA-TR-610, 1937. https://ntrs.nasa.gov/api/citations/19930091685/downloads/19930091685.pdf

THEODORSEN T. Theory of wing sections of arbitrary shape[R ] . NACA-TR-411, 1931. https://ntrs.nasa.gov/api/citations/19930091485/downloads/19930091485.pdf

Aircraft Design Manual editorial committee. Aircraft design manual, Volume 6, aerodynamic design[M]. Aviation Industry Press, 2002.

JACOBS E N. Preliminary report on laminar-flow airfoils and new methods adopted for airfoil and boundary-layer investigations[R ] . NACA-WR-L-345, 1939. https://ntrs.nasa.gov/api/citations/19930092782/downloads/19930092782.pdf

ABBOTT I H, VON DOENHOFF A E, STIVERS JR L S. Summary of airfoil data[R ] . NACA-TR-824, NASA, 1945. https://ntrs.nasa.gov/api/citations/19930092747/downloads/19930092747.pdf

ABBOTT I H, VON DOENHOFF A E. Theory of wing sections: including a summary of airfoil data[M]. Dover Publications, 1959, 11.

TRUCKENBRODT E. A method of quadrature for calculation of the laminar and turbulent boundary layer in case of plane and rotationally symmetrical flow[R ] . NACA-TM-1379, 1955. https://ntrs.nasa.gov/api/citations/19930093851/downloads/19930093851.pdf

WORTMANN F X. Progress in the design of low drag aerofoils[M]//Boundary Layer and Flow Control. Amsterdam: Elsevier, 1961: 748-770. doi: 10.1016/b978-1-4832-1323-1.50007-5

HARRIS C D. NASA supercritical airfoils: A matrix of family-related airfoils[R ] . NASA-TP-2969, NASA, 1990. https://ntrs.nasa.gov/api/citations/19900007394/downloads/19900007394.pdf

WHICOMB R T. Review of NASA supercritical airfoils[C]//9th International Council of the Aeronautical Sciences Congress, 1974. ICAS PAPER 74-10.

HARRIS C D. Aerodynamic characteristics of 10 percent thick NASA supercritical airfoils with different aft camber[R ] . NASA-TM-X-2977, NAS 1.15: X-72007, 1975. https://ntrs.nasa.gov/api/citations/19830002808/downloads/19830002808.pdf

HARRIS C D. Aerodynamic characteristics of a 14-percent-thick NASA supercritical airfoil designed for a normal-force coefficient of 0.7[R ] . NASA-TM-X-72711, NAS 1.15: X-72712, 1975. https://ntrs.nasa.gov/api/citations/19830013896/downloads/19830013896.pdf

PEARCEY H H. The aerodynamic design of section shapes for swept wings[M]//Advances in Aeronautical Sciences. Amsterdam: Elsevier, 1962: 277-322. doi: 10.1016/b978-0-08-006550-2.50021-1

CHEN Y C, ZHANG M H, ZHANG M, et al. Review of large civil aircraft aerodynamic design[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(1): 522759. (in Chinese)

SOMERS D M. Subsonic natural-laminar-flow airfoils[M]// BARNWELL R W, HUSSAINI M Y, Eds. Natural laminar flow and laminar flow control. Springer New York, 1992: 143-176.

MCGHEE R J, BEASLEY W D, WHITCOMB R T. NASA low-and medium-speed airfoil development[R]. NASA-TM-78709, 1979. https://ntrs.nasa.gov/api/citations/19800012809/downloads/19800012809.pdf

NAEGELE H, EPPLER R. Plastic sailplane FS-24 phoenix[J]. Soaring, 1958, 22: 2-5.

HANSON P W. Science and technology of low speed and motorless flight[R ] . NASA-CP-2085-PT-2, NASA, 1979, 131-153. https://ntrs.nasa.gov/api/citations/19790015718/downloads/19790015718.pdf

EPPLER R, SOMERS D M. A computer program for the design and analysis of low-speed airfoils[R ] . NASA-TM-80210, 1980. https://ntrs.nasa.gov/api/citations/19800020753/downloads/19800020753.pdf

EPPLER R. Airfoil data[M]//Airfoil Design and Data. Berlin, Heidelberg: Springer Berlin Heidelberg, 1990: 163-512. doi: 10.1007/978-3-662-02646-5_6

DOENHOFF A E V, ABBOTT F T. The Langley two-dimensional low-turbulence pressure tunnel[R ] . NACA-TN-1283, 1947. https://ntrs.nasa.gov/api/citations/19930081899/downloads/19930081899.pdf

MCGHEE R J, BEASLEY W D, FOSTER J M. Recent modifications and calibration of the Langley low-turbulence pressure tunnel[R ] . NASA-TP-2328, 1984. https://ntrs.nasa.gov/api/citations/20020043801/downloads/20020043801.pdf

SOMERS D M. Design and experimental results for a natural-laminar-flow airfoil for general aviation applications[R ] . NASA-TP-1861, 1981. https://ntrs.nasa.gov/api/citations/19810015487/downloads/19810015487.pdf

PAYNE H E. Laminar flow rethink-using composite structure[R]. SAE Technical Paper 760473, 1976. doi: 10.4271/760473

PFENNINGER W. Investigations on reductions of friction on wings, in particular by means of boundary layer suction[M ] . NACATM-1181, 1947. https://ufdc.ufl.edu/AA00009311/00001

BEFUS J, LATAS J, NELSON E, et al. In-flight measurements of lift, drag, and pitching moments on an advanced NLF wing on a Cessna Model T210[C]//NASA Symposium on NLF and LFC Research, 1987.

LABRUJERE T E, LOEVE W, SLOOFF J W. An approximate method for the determination of the pressure distribution on wings in the lower critical speed range[R]. NLR MP 68005 U, National Aerospace Laboratory NLR, 1968.

SOMERS D M, HORSTMANN K H. Design of a medium-speed natural-laminar-flow airfoil for commuter aircraft applications[J]. DFVLR IB, 1985: 129-85.

VIKEN J K, WATSON-VIKEN S A, PFENNINGER W, et al. Design of the low-speed NLF(1)-0414F and the high-speed HSNLF(1)-0213 airfoils with high-lift systems[R ] //Research in Natural Laminar Flow and Laminar-Flow Control, Part 3. N90-12540, 1987. https://ntrs.nasa.gov/api/citations/19900003224/downloads/19900003224.pdf

SEWALL W G, MCGHEE R J, HAHNE D E, et al. Wind tunnel results of the high-speed NLF(1)-0213 airfoil[R ] //Research in Natural Laminar Flow and Laminar-Flow Control, Part 3. N90-12542, 1987. https://ntrs.nasa.gov/api/citations/19900003226/downloads/19900003226.pdf

KOSS D, STEINBUCH M, SHEPSHELOVICH M. . Design and experimental evaluation of a high-lift, mild-stall airfoil[C]//12th Applied Aerodynamics Conference, Colorado Springs, CO, USA. Reston, Virigina: AIAA, 1994. AIAA-1994-1867. doi: 10.2514/6.1994-1867

MAUGHMER M D, SOMERS D M. Design and experimental results for a high-altitude, long-endurance airfoil[J]. Journal of Aircraft, 1989, 26(2): 148-153. DOI:10.2514/3.45736

EPPLER R, SOMERS D M. Airfoil design for Reynolds numbers between 50, 000 and 500, 000[R]. NASA, 1985.

BANAL L F, UBANDO A T. Lift enhancement of the LRN 1015 airfoil using a gurney flap: a computational fluid dynamics investigation[J]. Journal of Computational Innovations and Engineering Applications, 2017, 2(1): 18-26.

CRANE H L, MCGHEE R J, KOHLMAN D L. Applications of advanced aerodynamic technology to light aircraft[C]//SAE Technical Paper Series, 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1973. doi: 10.4271/730318

VAN TASSEL D. Studies of a new family of general aviation airfoils[C]//12th Annual Meeting and Technical Display, Washington, DC, USA. Reston, Virigina: AIAA, 1976. AIAA-1976-0217. doi: 10.2514/6.1976-217

QIAO Z D. Design of supercritical airfoils with natural laminar flow[J]. Experiments and Measurements in Fluid Mechanics, 1998, 12(4): 24-31. (in Chinese)

HUA J, ZHANG Z Y, SHI N G, et al. Numerical design method for modern NLF airfoils[J]. Acta Aerodynamica Sinica, 1993, 11(1): 57-63. (in Chinese)

HUA J, ZHANG Z Y, G. REDEKER, et al. Aerodynamic analysis and modification design of npu airfoils[J]. Acta Aeronautica et Astronautica Sinica, 1989, 10(4): 180-183. (in Chinese)

ZHANG Z Y, ZHAN H. [J]. NPU-ASN-1 airfoil for long-endurance airplane[J]. Journal of Northwestern Polytechnical University, 1999, 17(B12): 36-38. (in Chinese)

KONG F M, HUA J, XIANG J W, et al. Design and research of high-lift mild-stall airfoils[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(2): 235-237. (in Chinese)

YANG W. Development of future fighters[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(6): 524377. (in Chinese)

WANG C, GAO Z H. Refined aerodynamic design optimization of a wing with small aspect ratio[J]. SCIENTIA SINICA Technologica, 2015, 45(6): 643-653. (in Chinese)

GAO Z H, WANG C, HUANG J T. HDMR-based surrogate model for high dimensional aerodynamic design problems[C]//16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Dallas, TX. Reston, Virginia: AIAA, 2015. AIAA-2015-3094. doi: 10.2514/6.2015-3094

WANG C. Research on surrogate-based efficient aerodynamic optimization and many-objective problems[D]. Xi'an: Northwestern Polytechnical University, 2018 (in Chinese).

WANG C, GAO Z H, HUANG J T, et al. Smoothing methods based on coordinate transformation in a linear space and application in airfoil aerodynamic design optimization[J]. Science China Technological Sciences, 2015, 58(2): 297-306. DOI:10.1007/s11431-014-5745-4

李广义. 未来大型客机发展展望[J]. 国防科技工业, 2008(6): 24-29.

蔡向阳, 董树军, 宋虹兴. 无人侦察机装备发展现状及趋势[J]. 飞航导弹, 2010(4): 33-36.

LIEBECK R H. Design of the blended wing body subsonic transport[J]. Journal of Aircraft, 2004, 41(1): 10-25. DOI:10.2514/1.9084

MIALON B, FOL T, BONNAUD C. Aerodynamic optimization of subsonic flying wing configurations[C]//20th AIAA Applied Aerodynamics Conference, St. Louis, Missouri. Reston, Virigina: AIAA, 2002. AIAA-2002-2931. doi: 10.2514/6.2002-2931

WANG H F, BAI J Q. Design essentials research of the flying-wing configuration[J]. Science Technology and Engineering, 2009, 9(12): 3570-3573. (in Chinese)

ZHANG B Q, LUO L, CHEN Z L, et al. On stealth airfoil optimization design for flying wing configuration[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(4): 957-967. (in Chinese)

XIA L, ZHANG X, YANG M H, et al. Airfoil aerodynamic stealth integrated design for a flying wing configuration[J]. Journal of Northwestern Polytechnical University, 2017, 35(5): 821-826. (in Chinese)

LI P F, ZHANG B Q, TAO Y J, et al. Center body airfoil design for blended wing body configuration[J]. Journal of Northwestern Polytechnical University, 2018, 36(2): 203-210. (in Chinese)

ROMAN D, GILMORE R, WAKAYAMA S. Aerodynamics of high-subsonic blended-wing-body configurations[C]//41st Aerospace Sciences Meeting and Exhibit, Reno, Nevada. Reston, Virginia: AIAA, 2003. AIAA-2003-554 doi: 10.2514/6.2003-554

JIAO Z H, ZHANG B Q, SHEN D. Investigation on the effects of geometric parameters on airfoils' stealth characteristics[J]. Mechanical Science and Technology for Aerospace Engineering, 2012, 31(12): 1980-1987. (in Chinese)

CHEN X, BAI J Q, LI Q. Airfoil optimization of a stealth flying wind aerial vehicle[J]. Aeronautical Computing Technique, 2013, 43(6): 46-49, 53. (in Chinese)

LI Q, GUO Z D, LEI W T, et al. Study on supercritical airfoil of blended wing body[J]. Acta Aerodynamica Sinica, 2017, 35(4): 579-586. (in Chinese)

ZHENG C Y, HUANG J T, ZHOU Z, et al. Multidisciplinary optimization design of high dimensional target space for flying wing airfoil[J]. Acta Aerodynamica Sinica, 2017, 35(4): 587-597. (in Chinese)

PAMBAGJO T, NAKAHASHI K, OBAYASHI S, et al. Aerodynamic design of a medium size blended-wing-body airplane[C]//39th Aerospace Sciences Meeting and Exhibit, Reno, NV, USA. Reston, Virigina: AIAA, 2001. AIAA-2001-0129. doi: 10.2514/6.2001-129

PEIGIN S, EPSTEIN B. Computational fluid dynamics driven optimization of blended wing body aircraft[J]. AIAA Journal, 2006, 44(11): 2736-2745. DOI:10.2514/1.19757

HILEMAN J I, SPAKOVSZKY Z S, DRELA M, et al. Airframe design for silent fuel-efficient aircraft[J]. Journal of Aircraft, 2010, 47(3): 956-969. DOI:10.2514/1.46545

QIN N, VAVALLE A, MOIGNE A L, et al. Aerodynamic studies for blended wing body aircraft[C]//9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Atlanta, Georgia, 2002. AIAA-2002-5448. doi: 10.2514/6.2002-5448

WANG H J, LI J, ZHOU Z. Airfoil and wing layout design for a certain flying wing UAV (unmanned air vehicle)[J]. Journal of Northwestern Polytechnical University, 2011, 29(5): 789-793. (in Chinese)

GAO Z H, ZHAO K, WANG C. Aerodynamic shape optimization of BWB aircraft based on multizone collaborative optimization design method[C]//33rd AIAA Applied Aerodynamics Conference, Dallas, TX. Reston, Virginia: AIAA, 201. AIAA-2015-2878. doi: 10.2514/6.2015-2878

ZHOU L, HUANG J T, GAO Z H, et al. Three-dimensional aerodynamic/stealth optimization based on adjoint sensitivity analysis for scattering problem[J]. AIAA Journal, 2020, 58(6): 2702-2715. DOI:10.2514/1.j059136

ZHANG W, GAO Z H, ZHOU L, et al. Research on multimodality in aerodynamic/stealth airfoil design optimization[C]//2021 12th International Conference on Mechanical and Aerospace Engineering (ICMAE), Athens, Greece. IEEE, 2021: 384-393. doi: 10.1109/ICMAE52228.2021.9522566

WANG C, GAO Z H, ZHANG W, et al. Efficient surrogate-based aerodynamic design optimization method with adaptive design space expansion[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(7): 121745. (in Chinese)

ZHANG W, GAO Z H, ZHOU L, et al. Adaptive parameterization method for surrogate-based global optimization[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(10): 123815. (in Chinese)

WANG K L, ZHU X P, ZHOU Z, et al. Studying optimization design of low Reynolds number airfoil using transition model[J]. Journal of Northwestern Polytechnical University, 2015, 33(4): 580-587. (in Chinese)

DRELA M. XFOIL: an analysis and design system for low Reynolds number airfoils[C ] //Low Reynolds Number Aerodynamics, University of Notre Dame , 1989. https://www.researchgate.net/publication/235994182_XFOIL_An_Analysis_and_Design_System_for_Low_Reynolds_Number_Airfoils doi: 10.1007/978-3-642-84010-4_1

SELIG M S. Summary of Low-Speed Airfoil Data[R]. SoarTech Publications, 1995.

WANG K L, ZHOU Z, GAN W B, et al. Studying aerodynamic performances of the low-Reynolds-number airfoil of solar energy UAV[J]. Journal of Northwestern Polytechnical University, 2014, 32(2): 163-168. (in Chinese)

司江涛, 赵克良, 韩先锂. 高亚音速低雷诺数翼型研究[J]. 飞机工程, 2003(2): 26-29.

WANG H T, ZHU Y Z, CHE X K, et al. Separation bubble and aerodynamic characteristics of S1223 airfoil at low Reynolds numbers[J]. Acta Aerodynamica Sinica, 2021, 39(3): 90-98. (in Chinese)

ZHANG Y F, SONG B F, LI Z K. Aerodynamic optimization design and experiment study for a high-lift airfoil[J]. Flight Dynamics, 2006, 24(4): 70-72. (in Chinese)

CHEN Y H, CHEN Z H, FAN B C, et al. Electro-magnetic control of the flow past a foil at a low Reynolds number[J]. Acta Aerodynamica Sinica, 2007, 25(z2): 91-96. (in Chinese)

CHEN X K, GUO Z, YI F, et al. Aerodynamic shape optimization and design of airfoils with low Reynolds number[J]. Acta Aerodynamica Sinica, 2014, 32(3): 300-307. (in Chinese)

CHEN X K, GUO Z, YI F, et al. Single and multi-point aerodynamic shape optimization of low Reynolds number airfoils[C]//14th Chinese Conference on System Simulation Technology and Application, 2012 (in Chinese).

ZHAO Z M, LI J. Optimal design of high-lift airfoil design based on genetic algorithm combined with inverse design method[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2008, 28(5): 183-187. (in Chinese)

ZHAO H, GAO Z H, XU F, et al. Review of robust aerodynamic design optimization for air vehicles[J]. Archives of Computational Methods in Engineering, 2019, 26(3): 685-732. DOI:10.1007/s11831-018-9259-2

ZHAO H, GAO Z H, XU F, et al. An efficient adaptive forward-backward selection method for sparse polynomial chaos expansion[J]. Computer Methods in Applied Mechanics and Engineering, 2019, 355: 456-491. DOI:10.1016/j.cma.2019.06.034

ZHAO H, GAO Z H, GAO Y, et al. Effective robust design of high lift NLF airfoil under multi-parameter uncertainty[J]. Aerospace Science and Technology, 2017, 68: 530-542. DOI:10.1016/j.ast.2017.06.009

ZHAO H, GAO Z H, WANG C, et al. Robust design of high speed natural-laminar-flow airfoil for high lift[C]//55th AIAA Aerospace Sciences Meeting, Grapevine, Texas. Reston, Virginia: AIAA, 2017. AIAA-2017-1414 doi: 10.2514/6.2017-1414

BALAKUMAR P, KING R. Receptivity and transition of supersonic boundary layers over swept wings[C]//48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida. Reston, Virginia: AIAA, 2010. AIAA-2010-1454. doi: 10.2514/6.2010-1454

FUJINO M, YOSHIZAKI Y, KAWAMURA Y. Natural-laminar-flow airfoil development for a lightweight business jet[J]. Journal of Aircraft, 2003, 40(4): 609-615. DOI:10.2514/2.3145

ZHU J, GAO Z H, ZHAN H, et al. A high-speed nature laminar flow airfoil and its experimental study in wind tunnel with nonintrusive measurement technique[J]. Chinese Journal of Aeronautics, 2009, 22(3): 225-229. DOI:10.1016/S1000-9361(08)60091-6

SEITZ A, KRUSE M, WUNDERLICH T, et al. The DLR project LamAiR: design of a NLF forward swept wing for short and medium range transport application[C]//29th AIAA Applied Aerodynamics Conference, Honolulu, Hawaii. Reston, Virginia: AIAA, 2011. AIAA-2011-3526. doi: 10.2514/6.2011-3526

STREIT T, WICHMANN G, VON KNOBLAUCH ZU HATZBACH F, et al. Implications of conical flow for laminar wing design and analysis[C]//29th AIAA Applied Aerodynamics Conference, Honolulu, Hawaii. Reston, Virginia: AIAA, 2011. AIAA-2011-3808. doi: 10.2514/6.2011-3808

AMOIGNON O, PRALITS J, HANIFI A, et al. Shape optimization for delay of laminar-turbulent transition[J]. AIAA Journal, 2006, 44(5): 1009-1024. DOI:10.2514/1.12431

DRIVER J, ZINGG D W. Numerical aerodynamic optimization incorporating laminar-turbulent transition prediction[J]. AIAA Journal, 2007, 45(8): 1810-1818. DOI:10.2514/1.23569

RASHAD R, ZINGG D W. Aerodynamic shape optimization for natural laminar flow using a discrete-adjoint approach[J]. AIAA Journal, 2016, 54(11): 3321-3337. DOI:10.2514/1.J054940

LEE J D, JAMESON A. NLF airfoil and wing design by adjoint method and automatic transition prediction[C]//27th AIAA Applied Aerodynamics Conference, San Antonio, Texas. Reston, Virginia: AIAA, 2009. AIAA-2009-3514. doi: 10.2514/6.2009-3514

MA X Y, ZHANG Y J, DUAN Z Y, et al. Study of aerodynamic shape optimization for natural laminar wing[J]. Acta Aerodynamica Sinica, 2015, 33(6): 812-817. (in Chinese)

CAMERON L, EARLY J, MCROBERTS R. Metamodel assisted multi-objective global optimisation of natural laminar flow aerofoils[C]//29th AIAA Applied Aerodynamics Conference, Honolulu, Hawaii. Reston, Virginia: AIAA, 2011. AIAA-2011-3001. doi: 10.2514/6.2011-3001

HAN Z H, DENG J, LIU J, et al. Design of laminar supercritical airfoils based on Navier–Stokes equations[C ] //28th International Congress of the Aeronautical Sciences, 2012. https://www.researchgate.net/publication/290032856_Design_of_laminar_supercritical_airfoils_based_on_Navier-Stokes_equations

HAN Z H, CHEN J, ZHANG K S, et al. Aerodynamic shape optimization of natural-laminar-flow wing using surrogate-based approach[J]. AIAA Journal, 2018, 56(7): 2579-2593. DOI:10.2514/1.J056661

CHEN J, SONG W P, ZHU Z, et al. A hybrid inverse/direct optimization design method for transonic laminar flow airfoil[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(12): 122219. (in Chinese)

CHI J B, HAN Z H, FAN T L, et al. Hybrid inverse/optimization design approach for transonic natural-laminar-flow airfoils[C]//AIAA Scitech 2019 Forum, San Diego, California. Reston, Virginia: AIAA, 2019. AIAA-2019-1475. doi: 10.2514/6.2019-1475

ZHANG Y F, FANG X M, CHEN H X, et al. Supercritical natural laminar flow airfoil optimization for regional aircraft wing design[J]. Aerospace Science and Technology, 2015, 43: 152-164. DOI:10.1016/j.ast.2015.02.024

SARIC W S, REED H L, WHITE E B. Stability and transition of three-dimensional boundary layers[J]. Annual Review of Fluid Mechanics, 2003, 35(1): 413-440. DOI:10.1146/annurev.fluid.35.101101.161045

XU Z M, HAN Z H, CHI J B, et al. Crossflow instability analysis for swept laminar flow wings using crossflow pressure gradient[J]. AIAA Journal, 2021, 59(8): 2878-2889. DOI:10.2514/1.J059971

REDEKER G, HORSTMANN K H, KOSTER H, et al. Investigations on high Reynolds number laminar flow airfoils[J]. Journal of Aircraft, 1988, 25(7): 583-590. DOI:10.2514/3.45627

LYNDE M N, CAMPBELL R L. Computational design and analysis of a transonic natural laminar flow wing for a wind tunnel model[C]//35th AIAA Applied Aerodynamics Conference, Denver, Colorado. Reston, Virginia: AIAA, 2017. AIAA-2017-3058. doi: 10.2514/6.2017-3058

LYNDE M N, CAMPBELL R L, VIKEN S A. Additional findings from the common research model natural laminar flow wind tunnel test[C]//AIAA Aviation 2019 Forum, Dallas, Texas. Reston, Virginia: AIAA, 2019. AIAA-2019-3292. doi: 10.2514/6.2019-3292

XU Z M, HAN Z H, SONG W P. Natural-laminar-flow airfoil design optimization considering crossflow instability when configured on a swept wing[C ] // 32nd International Council of the Aeronuautical Sciencea, 2021. https://www.icas.org/ICAS_ARCHIVE/ICAS2020/data/papers/ICAS2020_0472_paper.pdf

YOSHIDA K. Supersonic drag reduction technology in the scaled supersonic experimental airplane project by JAXA[J]. Progress in Aerospace Sciences, 2009, 45(4-5): 124-146. DOI:10.1016/j.paerosci.2009.05.002

LYNDE M N, CAMPBELL R L. Expanding the natural laminar flow boundary for supersonic transports[C]//34th AIAA Applied Aerodynamics Conference, Washington, D. C. . Reston, Virginia: AIAA, 2016. AIAA-2016-4327. doi: 10.2514/6.2016-4327

UEDA Y, YOSHIDA K, MATSUSHIMA K, et al. Supersonic natural-laminar-flow wing-design concept at high-Reynolds-number conditions[J]. AIAA Journal, 2014, 52(6): 1294-1306. DOI:10.2514/1.J052555

VERMEERSCH O, YOSHIDA K, UEDA Y, et al. Natural laminar flow wing for supersonic conditions: Wind tunnel experiments, flight test and stability computations[J]. Progress in Aerospace Sciences, 2015, 79: 64-91. DOI:10.1016/j.paerosci.2015.07.003

IULIANO E, DIN I S E, DONELLI R, et al. Natural laminar flow design of a supersonic transport jet wing body[C]//47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition, Orlando, Florida. Reston, Virginia: AIAA, 2009. AIAA-2009-1279. doi: 10.2514/6.2009-1279

IULIANO E, QUAGLIARELLA D, DONELLI R S, et al. Design of a supersonic natural laminar flow wing-body[J]. Journal of Aircraft, 2011, 48(4): 1147-1162. DOI:10.2514/1.c031039

UENO A, SUZUKI K. CFD-based shape optimization of hypersonic vehicles considering transonic aerodynamic performance[C]//46th AIAA Aerospace Sciences Meeting and Exhibit, 2008: 288

UENO A, SUZUKI K. Two-dimensional shape optimization of hypersonic vehicles considering transonic aerodynamic performance[J]. Transactions of the Japan Society for Aeronautical and Space Sciences, 2009, 52(176): 65-73. DOI:10.2322/tjsass.52.65

SUN X C, HAN Z H, LIU F, et al. Design and analysis of hypersonic vehicle airfoil/wing at wide-range Mach numbers[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(6): 121737. (in Chinese)

LIU F, HAN Z H, ZHANG Y, et al. Surrogate-based aerodynamic shape optimization of hypersonic flows considering transonic performance[J]. Aerospace Science and Technology, 2019, 93: 105345. DOI:10.1016/j.ast.2019.105345

ZHANG Y, HAN Z H, LIU F, et al. Multi-objective aerodynamic shape optimization of wide-Mach-number-range airfoil[J]. Physics of Gases, 2019, 4(4): 26-40. (in Chinese)

ZHANG Y, HAN Z H, LI U F, et al. Aerodynamic design optimization of hypersonic wing over wide Mach-number range considering lift matching[C ] // 32nd International Council of the Aeronuautical Sciencea, 2021. https://www.icas.org/ICAS_ARCHIVE/ICAS2020/data/papers/ICAS2020_0476_paper.pdf

PHILIPPE J J. 30 Years of Rotorcraft Aeromechanics Research at ONERA[R]. ONERA TP 2007-33, 2007.

CHERNYSHEV S, GOLOVKIN M. Current state and progress in reseach of rotorcraft aerodynamics at TSAGI[C ] //35th European Rotorcraft Forum, 2009. http://toc.proceedings.com/07271webtoc.pdf

PASSE B J, SRIDHARAN A, BAEDER J D. Computational investigation of coaxial rotor interactional aerodynamics in steady forward flight[C]//33rd AIAA Applied Aerodynamics Conference, Dallas, TX. Reston, Virginia: AIAA, 2015. AIAA-2015-2883. doi: 10.2514/6.2015-2883

高正红. 通过局部参数化修形控制旋翼翼型俯仰力矩等设计新方法: CN106777495A[P]. 2017-05-13.

杨旭东, 彭小康, 高正红, 等. 一种全工况条件下高升力低力矩特性12%厚度旋翼翼型: CN106741925A[P]. 2017-05-31.

宋文萍, 卜月鹏, 韩忠华, 等. 一种全工况条件下的高升阻比低力矩特性9%厚度旋翼翼型: CN106741924A[P]. 2017-05-31.

杨旭东, 彭小康, 高正红, 等. 一种全工况条件下高升力低力矩特性7%厚度旋翼翼型: CN106741923A[P]. 2017-05-31.

ZHAO K. Complex aerodynamic optimization and robust design method based on computational fluid dynamics[D]. Xi'an: Northwestern Polytechnical University, 2015 (in Chinese).

SUN W, GAO Z H, DU Y M, et al. Mechanism of unconventional aerodynamic characteristics of an elliptic airfoil[J]. Chinese Journal of Aeronautics, 2015, 28(3): 687-694. DOI:10.1016/j.cja.2015.03.009

HAN S Q, SONG W P, HAN Z H, et al. Hybrid inverse/optimization design method for rigid coaxial rotor airfoils considering reverse flow[J]. Aerospace Science and Technology, 2019, 95: 105488. DOI:10.1016/j.ast.2019.105488

赵佳祥, 宋文萍, 韩忠华, 等. 应用于高速直升机旋翼反流区的类椭圆翼型: CN109229364B[P]. 2019-06-11.

韩少强, 宋文萍, 韩忠华, 等. 用于高速直升机旋翼桨根的非对称双钝头翼型及设计方法: CN111717381B[P]. 2021-10-08.

高正红, 赵欢, 夏露. 一种具有低阻高发散马赫数的共轴双旋翼高速直升机桨尖翼型: CN112572787A[P]. 2021-03-30.

李萍, 庄开莲, 李静. 国外直升机旋翼翼型研究综述[J]. 直升机技术, 2007(3): 103-109.

SUN J F, LU F S, HUANG Y, et al. Rotor airfoil aerodynamic design and evaluation software HRADesign[J]. Acta Aerodynamica Sinica, 2021, 39(4): 59-68. (in Chinese)

WANG Q, ZHAO Q J. Synthetical optimization design of rotor airfoil by genetic algorithm[J]. Journal of Aerospace Power, 2016, 31(6): 1486-1495. (in Chinese)

ZHAO Q J, WANG Q, ZHAO G Q. New optimization design method for rotor airfoil considering steady-unsteady characteristics[J]. Journal of Nanjing University of Aeronautics Astronautics, 2014, 46(3): 355-363. (in Chinese)

QIAN R Z, QIAO Z D, CHEN Y C, et al. Rotor airfoil optimization design using Navier-Stokes equations[J]. Flight Dynamics, 2004, 22(1): 26-29. (in Chinese)

HUANG H S, YANG X D. Optimum shape design of rotor airfoils via control theory[J]. Aeronautical Computing Technique, 2010, 40(4): 22-26. (in Chinese)

YANG H, SONG W P, HAN Z H, et al. Multi-objective and multi-constrained optimization design for a helicopter rotor airfoil[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(7): 1218-1226. (in Chinese)

SUN J F, LIU G, JIANG X, et al. Research of rotor airfoil design optimization based on the Kriging model[J]. Acta Aerodynamica Sinica, 2013, 31(4): 437-441. (in Chinese)

VU N A, LEE J W, SHU J I. Aerodynamic design optimization of helicopter rotor blades including airfoil shape for hover performance[J]. Chinese Journal of Aeronautics, 2013, 26(1): 1-8. DOI:10.1016/j.cja.2012.12.008

SHANG K M, ZHAO Q J, ZHAO G Q, et al. Inverse design analysis on helicopter rotor airfoils and aerodynamic shapes[J]. Journal of Nanjing University of Aeronautics Astronautics, 2010, 42(5): 550-556. (in Chinese)

LI S W, XIONG J Q, WANG X L. New helicopter rotor aerodynamic characteristics and layout analysis[J]. Journal of Nanjing University of Aeronautics Astronautics, 2020, 52(2): 318-333. (in Chinese)

MANI K, LOCKWOOD B A, MAVRIPLIS D J. Adjoint-based unsteady airfoil design optim ization with application to dynamic stall[C ] //American Helicopter Society 68th Annual Forum, 2012. http://scientific-sims.com/cfdlab/Dimitri_Mavriplis/HOME/assets/papers/AHS.2012.paper.pdf

WANG Q, ZHAO Q J. Rotor airfoil profile optimization for alleviating dynamic stall characteristics[J]. Aerospace Science and Technology, 2018, 72: 502-515. DOI:10.1016/j.ast.2017.11.033

YU B P, LI G H, XIE L, et al. Dynamic stall optimization design of rotor airfoil based on surrogate model[J]. Journal of Zhejiang University (Engineering Science), 2020, 54(4): 833-842. (in Chinese)

KONG W H, CHEN R L, SUN Z H. Numerical investigation of dynamic stall on rotor airfoil in low-speed flow[J]. Journal of Nanjing University of Aeronautics Astronautics, 2018, 50(2): 213-220. (in Chinese)

ZHANG S L, YANG X D, SONG B F, et al. Experimental investigation of lift enhancement and drag reduction of rotor airfoil using co-flow jet concept[J]. Advances in Aeronautical Science and Engineering, 2021, 12(4): 44-51, 67. (in Chinese)

MA Y Y, ZHAO Q J, ZHAO G Q. New combinational active control strategy for improving aerodynamic characteristics of airfoil and rotor[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2020, 234(4): 977-996. DOI:10.1177/0954410019893193

YANG X D, JIANG W R, ZHANG S L. Analysis of co-flow jet effect on dynamic stall characteristics applying to rotor airfoils[J]. IOP Conference Series: Materials Science and Engineering, 2019, 491: 012010. DOI:10.1088/1757-899x/491/1/012010

ZHAO Q J, MA Y Y, ZHAO G Q. Parametric analyses on dynamic stall control of rotor airfoil via synthetic jet[J]. Chinese Journal of Aeronautics, 2017, 30(6): 1818-1834. DOI:10.1016/j.cja.2017.08.011

ZHAO G Q, ZHAO Q J. Parametric analyses for synthetic jet control on separation and stall over rotor airfoil[J]. Chinese Journal of Aeronautics, 2014, 27(5): 1051-1061. DOI:10.1016/j.cja.2014.03.023

XU H Y, XING S L, YE Z Y, et al. Dynamic stall suppression for rotor airfoil based on inflatable leading edge technology[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(6): 120799. (in Chinese)

ZHAO G Q. Investigations on CFD simulation and active flow control for unsteady dynamic stall of helicopter rotor[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2015 (in Chinese).

ZHANG W, LIN Y F, CHEN P J. The investigation of active control technology in airfoil flow field based on the synthetic jet[J]. Helicopter Technique, 2010(1): 15-20. (in Chinese)

HAN Z H, SONG W P, QIAO Z D. Numerical simulation of active dynamic stall control on an OA212 rotor airfoil[J]. Acta Aerodynamica Sinica, 2009, 27(6): 639-644. (in Chinese)

WU X M, MU X W. A perspective of the future development of key helicopter technologies[J]. Acta Aerodynamica Sinica, 2021, 39(3): 1-10. (in Chinese)

COLOZZA A. Initial feasibility assessment of a high altitude long endurance airship[R ] . NASA/CR-212724, 2003. https://ntrs.nasa.gov/api/citations/20040021326/downloads/20040021326.pdf

COLOZZA A. APEX 3D propeller test preliminary design[R ] . NASA/CR-2002-211866, 2002. https://ntrs.nasa.gov/api/citations/20020082943/downloads/20020082943.pdf

QIAO Z D, ZHONG B W, JI Z. An integrated design method of low noise contrarotating propellers[J]. Journal of Northwestern Polytechnical University, 1997, 15(1): 37-42(in Chinese)

ZHANG S L, YANG X D, SONG B F, et al. Aerodynamic design of a novel low-Reynolds-number airfoil for near space propellers[J ] . International Journal of Aerospace System Engineering, 2015, 2(1): 53-57. http://www.koreascience.kr/article/JAKO201508361186873.pdf

杨旭东, 张顺磊, 许建华, 等. 一种极低雷诺数高升阻比低速特殊勺型翼型: CN104118556A[P]. 2014-10-29.

XU J H, SONG W P, HAN Z H, et al. Effect of Mach number on high-subsonic and low-Reynolds-number flows around airfoils[J]. International Journal of Modern Physics B, 2020, 34(14n16): 2040112. DOI:10.1142/s0217979220401128

XU J H, LI H J, SONG W P, et al. An aerodynamic design method of propeller airfoils with geometric compatibility as constraints[C]//AIAA Aviation 2019 Forum, Dallas, Texas. Reston, Virginia: AIAA, 2019. AIAA-2019-3493. doi: 10.2514/6.2019-3493

XU J H, LI D, SONG W P, et al. Design optimization of airfoils at ultra-low Reynolds numbers[C ] // 32nd International Council of the Aeronuautical Sciencea, 2021. https://www.icas.org/ICAS_ARCHIVE/ICAS2020/data/papers/ICAS2020_0839_paper.pdf

刘沛清. 空气螺旋桨理论及其应用[M]. 北京: 北京航空航天大学出版社, 2006.

马蓉, 刘沛清, 胡颖. 临近空间飞行器螺旋桨低雷诺数高升力翼型综述[C]//庆祝中国力学学会成立50周年暨中国力学学会学术大会, 北京, 2007.

HAN Z H, SONG W P, GAO Y W. Design and wind-tunnel verification of large-size wind turbine airfoils[J]. Applied Mathematics and Mechanics, 2013, 34(10): 1012-1027. (in Chinese)

TANGLER J L, SOMERS D M. NREL airfoil families for HAWTS[R]. National Renewable Energy Laboratory, 1995. NREL/TP-442-7109. https://www.nrel.gov/docs/legosti/old/7109.pdf DOI:10.2172/10106095

FUGLSANG P, BAK C. Development of the Risø wind turbine airfoils[J]. Wind Energy, 2004, 7(2): 145-162. DOI:10.1002/we.117

BJORK A. Coordinates and Calculations for the FFA-W1-XXX, FFA-W2-XXX, FFA-W3-XXX series of airfoils for HAWTs[R ] . FFA TN 1990-15, Stockholm, Sweden, 1990. https://wind.nrel.gov/airfoils/Documents/FFA%20TN%201990-15%20v.1-2%20c.1.pdf

TIMMER W A, VAN ROOIJ R P J O M. Summary of the Delft university wind turbine dedicated airfoils[C ] //41st Aerospace Sciences Meeting and Exhibit, Reno, Nevada. Reston, Virginia: AIAA, 2003. AIAA 2003-0352. https://odonata-research.com/references/wind-turbine/AIAA-2003-0352.pdf doi: 10.2514/6.2003-352

QIAO Z D, SONG W P, GAO Y W. Design and experiment of the NPU-WA airfoil family for wind turbines[J]. Acta Aerodynamica Sinica, 2012, 30(2): 260-265. (in Chinese)

XU J H, HAN Z H, YAN X C, et al. Design optimization of a multi-megawatt wind turbine blade with the NPU-MWA airfoil family[J]. Energies, 2019, 12(17): 3330. DOI:10.3390/en12173330

BAI J Y, YANG K, LI H L, et al. Design of the horizontal axis wind turbine airfoil family[J]. Journal of Engineering Thermophysics, 2010, 31(4): 589-592. (in Chinese)

CHEN F H. Research on optimum design of wind turbine airfoils[D]. Beijing: North China Electric Power University, 2013. (in Chinese)

CHEN J, ZHANG S Q, WANG X D, et al. Dedicated wind turbine airfoil design based on the roughness sensitivity considerations[J]. Acta Aerodynamica Sinica, 2011, 29(2): 142-149. (in Chinese)

HUANG J X. Research on new wind turbine airfoils and their aerodynamic performances[D]. Shantou, China: Shantou University, 2001 (in Chinese).

SONG X C, CHEN J, DU G, et al. Parametric representation method for wind turbine airfoils[J]. Journal of Nanjing University of Aeronautics Astronautics, 2012, 44(3): 301-306. (in Chinese)

HAO L S, GAO Y W, WEI B B, et al. Numerical simulation of flow over bionic airfoil[J]. International Journal of Aerospace Engineering, 2021, 2021: 1-17. DOI:10.1155/2021/5556463

YANG Y X, YANG T H, BAI J Q, et al. Problems in optimization design of HLFC sweep wing[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(1): 121448. (in Chinese)

XU H Y, QIAO C L, YANG H Q, et al. Active circulation control on the blunt trailing edge wind turbine airfoil[J]. AIAA Journal, 2018, 56(2): 554-570. DOI:10.2514/1.j056223

XU J H, LI K, SONG W P, et al. Influence of co-flow jet key parameters on airfoil aerodynamic performance at low Reynolds number[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(8): 122018. (in Chinese)

ZHU L Q, SUN G K, LI H, et al. Intelligent and flexible morphing wing technology: a review[J]. Journal of Mechanical Engineering, 2018, 54(14): 28-42. (in Chinese)

BAI P, CHEN Q, XU G W, et al. Development status of key technologies and expectation about smart morphing aircraft[J]. Acta Aerodynamica Sinica, 2019, 37(3): 426-443. (in Chinese)

张尧, 张婉, 别大卫, 等. 智能变体飞行器研究综述与发展趋势分析[J]. 飞航导弹, 2021(6): 14-23.

XU Y T. Research on the development and key technology of smart morphing aircraft[J]. Tactical Missile Technology, 2017(2): 26-33, 46. (in Chinese)

NEAL D, GOOD M, JOHNSTON C, et al. Design and wind-tunnel analysis of a fully adaptive aircraft configuration[C]//45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics Materials Conference, Palm Springs, California. Reston, Virigina: AIAA, 2004. AIAA-2004-1727. doi: 10.2514/6.2004-1727

ELZEY D M, SOFLA A Y N, WADLEY H N G. A bio-inspired high-authority actuator for shape morphing structures[C]//Smart Structures and Materials 2003: Active Materials: Behavior and Mechanics, San Diego, CA. SPIE, 2003. doi: 10.1117/12.484745

CHEN Q. Preparation and control performances of soft actuator IPMC based on silver electrode[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2009 (in Chinese).

YIN M. Coordinated control of deformation and flight for morphing aircraft[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2016 (in Chinese).

LU Y P, HE Z. A survey of morphing aircraft control systems[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(10): 1906-1911. (in Chinese)

ZHU H, LIU W D, ZHAO C S. Morphing aircraft and its morph-driving techniques[J]. Machine Building Automation, 2010, 39(2): 8-14, 125. (in Chinese)

GAO Y F, LIU Z F, WANG X H. Study on the supersonic unsteady aerodynamic force for the morphing airfoil[J]. Acta Aerodynamica Sinica, 2014, 32(1): 69-76. (in Chinese)

崔尔杰, 白鹏, 杨基明. 智能变形飞行器的发展道路[J]. 航空制造技术, 2007, 50(8): 38-41.