[1]BARBARINO S, BILGEN O, AJAJ R M, et al.A review of morphing aircraft[J].Journal of intelligent material systems and structures, 2011, 22(9):823-877
[2]CHU LL, LI Q, GU F, et al.Design,modeling,and control of morphing aircraft: A review[J].Chinese Journal of Aeronautics, 2022, 35(5):220-246
[3]陈树生, 贾苜梁, 刘衍旭, 等.变体飞行器变形方式及气动布局设计关键技术研究进展[J].航空学报, 2024, 45(06):629595-629595
[4]Kulfan B M.Universal parametric geometry representation method[J].Journal of aircraft, 2008, 45(1):142-158
[5]Sederberg T W, Parry S R.Free-form deformation of solid geometric models[C]. Proceedings of the 13th annual conference on Computer graphics and interactive techniques. 1986: 151-160.
[6]Piegl L, Tiller W.The NURBS book[M]. Springer Science & Business Media, 2012.
[7]Sheng C, Allen C B.Efficient mesh deformation using radial basis functions on unstructured meshes[J].AIAA journal, 2013, 51(3):707-720
[8]Selim M M, Koomullil R P.Mesh deformation approaches–a survey[J].Journal of Physical Mathematics, 2016, 7(2):1-9
[9]Zhong Z, Rong M A, Lei H E, et al.An efficient large-scale mesh deformation method based on MPIOpenMP hybrid parallel radial basis function interpolation[J].Chinese Journal of Aeronautics, 2020, 33(5):1392-1404
[10]Gu X, Ciampa P D, Nagel B.An automated CFD analysis workflow in overall aircraft design applications[J].CEAS Aeronautical Journal, 2018, 9:3-13
[11]You K K, Ha J H, Lee S C.An Automated Aerodynamic Analysis System in Missile Based on Open-Source Software[J].International Journal of Aeronautical and Space Sciences, 2023, 24(3):592-605
[12]Jameson A.Aerodynamic design via control theory[J].Journal of scientific computing, 1988, 3:233-260
[13]Dwight R P, Brezillon J.Effect of approximations of the discrete adjoint on gradient-based optimization[J].AIAA journal, 2006, 44(12):3022-3031
[14]Kenway G K W, Mader C A, He P, et al.Effective adjoint approaches for computational fluid dynamics[J].Progress in Aerospace Sciences, 2019, 110:-
[15]陈海昕, 邓凯文, 李润泽.机器学习技术在气动优化中的应用[J].航空学报, 2019, 40(01):52-68
[16]Han Z H, Zimmermann, G?rtz S.Alternative cokriging method for variable-fidelity surrogate modeling[J].AIAA journal, 2012, 50(5):1205-1210
[17]Gu X, Ciampa P D, Nagel B.High fidelity aerodynamic optimization in distributed overall aircraft design[C]. 17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. 2016: 3508-3523.
[18]Brooks T R, Kenway G K W, Martins J R R A.Benchmark aerostructural models for the study of transonic aircraft wings[J].AIAA Journal, 2018, 56(7):2840-2855
[19]PHOENIX A A, MAXWELL J R, ROGERS R E.Mach 5–35 Morphing Waverider Accuracy and Aerodynamic Performance Evaluation[J].Journal of Aircraft, 2019, 56(5):2047-2061
[20]PHOENIX A A, ROGERS R E, MAXWELL J R, et al.Mach five to ten morphing waverider: control point study[J].Journal of Aircraft, 2019, 56(2):493-504
[21]PHOENIX A A, MAXWELL J R, ROGERS R E.Mach 5–35 morphing waverider accuracy and aerodynamic performance evaluation[J].Journal of Aircraft, 2019, 56(5):2047-2061
[22]DAI P, YAN B, HUANG W, et al.Design and aerodynamic performance analysis of a variable-sweep-wing morphing waverider[J].Aerospace Science and Technology, 2020, 98:-
[23]ZHAO Z, HUANG W, YAN B, et al.Design and high speed aerodynamic performance analysis of vortex lift waverider with a wide-speed range[J].Acta Astronautica, 2018, 151:848-863
[24]武宇飞, 龙腾, 史人赫, 等.跨域变体飞行器气动力热非层次多模型融合降阶方法[J].航空学报, 2023, 44(21):528259-528259
[25]FINCHAM J H S, FRISWELL M I.Aerodynamic optimisation of a camber morphing aerofoil[J].Aerospace Science and technology, 2015, 43:245-255
[26]WOODS B K S, FRISWELL M I.Preliminary investigation of a fishbone active camber concept[C]. Smart materials, adaptive structures and intelligent systems. American Society of Mechanical Engineers, 2012, 45103: 555-563.
[27]DEXL F, HAUFFE A, WOLF K.Multidisciplinary multi-objective design optimization of an active morphing wing section[J].[Structural and Multidisciplinary Optimization, 2020, 62:2423-2440
[28]LIU B, LIANG H, HAN Z H, et al.Surrogate-based aerodynamic shape optimization of a morphing wing considering a wide Mach-number range[J].[J].Aerospace Science and Technology, 2022, 124:-
[29]陈树生, 冯聪, 张兆康, 等.基于全局梯度优化方法的宽速域乘波-机翼布局气动设计[J].航空学报, 2024, 45(06):140-154
[30]DEB K, PRATAP A, AGARWAL S, et al.A fast and elitist multi-objective genetic algorithm: NSGA-II[J].IEEE Transactions on Evolutionary Computation, 2001, 6(2):182-197
[31]ROE P L.Approximate Riemann solvers,parameter vectors,and difference schemes[J].Journal of Computational Physics, 1981, 43(2):357-372
[32]CHEN R F, WANG Z J.Fast block lower-upper symetric Guass-Seidel scheme for arbitrary grid[J].AIAA Journal, 2000, 38(12):2238-2245
[33]VENKATAKRISHNAN.On the accuracy of limiters and convergence to steady state solutions[C]. 31st Aero-space Sciences Meeting. Reston: AIAA, 1993:
[34]KERMANI M, PLETT E.Modified entropy correction formula for the Roe scheme[C]. 39th Aerospace Sciences Meeting. Reston: AIAA, 2001.
[35]MENTER F R.Two-equation eddy-viscosity turbulence models for engineering applications[J].AIAA Journal, 1994, 32(8):1598-1605
[36]SEDERBERG T W, PARRY S R.Free-form deformation of solid geometric models[C]. Proceedings of the 13th annual conference on Computer graphics and interactive techniques. 1986: 151-160.
[37]WITTEVEEN J, BIJL H.Explicit mesh deformation using inverse distance weighting interpolation[M]. 19th AIAA Computational Fluid Dynamics. 2009: 3996.
[38]SEEGER M.Gaussian processes for machine learning[J].International journal of neural systems, 2004, 14(02):69-106
[39]KRIGE D G.A statistical approach to some basic mine valuation problems on the Witwatersrand[J].Journal of the Southern African Institute of Mining and Metallurgy, 1951, 52(6):119-139
[40]Morris M D, Mitchell T J.Exploratory designs for computational experiments[J].Journal of statistical planning and inference, 1995, 43(3):381-402
CJA