The DOI matches its Crossref record; 539 of the 548 references it cites were found in a registry or an index.
A review on design of experiments and surrogate models in aircraft real-time and many-query aerodynamic analyses
Overview
Integrity signals
Registry
Cites
Statistics
Verification
Claims the paper makes
Claims other papers make about this one
Each is checked against this paper’s own text: does it say what the citing paper says it does?
In the citing paper
“Aerodynamic efficiency improvements need turbulence modeling that is often computationally intensive and relies heavily on ML-based surrogate models [865].”
From Tackling climate change with machine learning (2023) · cites this paper as [865]
Citations
Cites
A Mathematical Theory of Communication
Shannon, C. E. (1948) · Bell System Technical Journal · doi:10.1002/j.1538-7305.1948.tb01338.x · Cited by 88,486
Cortes, C., & Vapnik, V. (1995) · Machine Learning · doi:10.1007/bf00994018 · Cited by 59,421
Genetic algorithms in search, optimization, and machine learning
(1989) · Choice Reviews Online · doi:10.5860/choice.27-0936 · Cited by 49,178
Adaptation in Natural and Artificial Systems
Holland, J. H. (1992) · The MIT Press eBooks · doi:10.7551/mitpress/1090.001.0001 · Cited by 47,340
Optimization by Simulated Annealing
Kirkpatrick, S., Gelatt, C. D., & Vecchi, M. P. (1983) · Science · doi:10.1126/science.220.4598.671 · Cited by 45,134
The Nature of Statistical Learning Theory
Vapnik, V. N. (1995) · doi:10.1007/978-1-4757-2440-0 · Cited by 39,138
Cortes, C., & Vapnik, V. N. (1995) · Machine Learning · doi:10.1023/a:1022627411411 · Cited by 34,565
Wu, Y., & Vapnik, V. N. (1999) · Technometrics · doi:10.2307/1271368 · Cited by 27,236
A logical calculus of the ideas immanent in nervous activity
McCulloch, W. S., & Pitts, W. (1943) · The Bulletin of Mathematical Biophysics · doi:10.1007/bf02478259 · Cited by 18,566
A new optimizer using particle swarm theory
Eberhart, R., & Kennedy, J. (2002) · MHS'95. Proceedings of the Sixth International Symposium on Micro Machine and Human Science · doi:10.1109/mhs.1995.494215 · Cited by 16,067
Research works printed but not linked: 40
- Koziel, 2011, 45(1–3), 33
- Viana, 2014, Metamodeling in multidisciplinary design optimization: how far have we really come?, J. Prog. Aerosp. Sci., 52, 670
- Koehler, 1996, Computer experiments, J. Prog. Aerosp. Sci., 261
- Finney, 1945, vol. 12, 291
- Fries, 1980, Minimum aberration 2k–p designs, Technometrics, 22, 601
- Rechtschaffner, 2005, Saturated fractions of 2n and 3n factorial designs, Technometrics, 9, 569
- Box, 1961, The 2k–p fractional factorial designs, Part I, Technometrics, 3, 311
- Box, 1961, The 2k–p fractional factorial designs, Part II, Technometrics, 3, 449
- Yue, 1999, Robust optimal designs for fitting approximately linear models, Stat. Sin., 9, 1053
- Owen, 1992, Randomly orthogonal arrays for computer experiments, integration and visualization, Stat. Sin., 2, 439
- Fang, 1980, The uniform design: application of number theoretic methods in experimental design, Acta Math. Appl. Sin., 3, 362
- S. Mak and V. R. Joseph, Minimax designs using clustering. J. Comput. Graph. Stat., submitted for publication, arxiv.org/abs/1602.03938. · arXiv
- B.G.M. Husslage, reportMaximin Designs for Computer Experiments. (Doctoral dissertation), Tilburg University, Tilburg, Netherlands.
- Husslage, 2006, vol. 18
- Yondo, 2016, A 2D numerical study of the influence of a priori sampling methods on surrogate models accuracy in aircraft aerodynamic design optimization, vol. 510
- Klein, 1983, vol. 2126
- Jouke H.S. de Baar, Thomas P. Scholcz, Clemens V. Verhoosel, Richard P. Dwight, Alexander H. van Zuijlen and Hester Bijl, Efficient uncertainty quantification with gradient-enhanced Kriging: applications in FSI, In J. Eberhardsteiner et al (eds.). European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2012), 51, Vienna, Austria, September 10-14, 2012.
- Le Gratiet, 2013, vol. 2
- Broomhead, 1988, Multivariate functional interpolation and adaptative networks, J. Complex Syst., 2, 321
- Quarteroni, 2014, vol. 9
- Kroll, 2012, CEAS Aeronaut. J., 151
- Loéve, 1945, Functions Aleatoire de Second Ordre, C. R. Acad. Sci. Paris, 220
- Obukbov, 1954, Statistical description of continuous fields, Tr. Geophys. Int. Akad. Nauk. SSSR, 24, 3
- Pougachev, 1953, General theory of the correlations of random functions, Izv. Akud. Nauk. SSSR, Set. Mat., 17
- Chen, 2012, Support-vector-machine-based reduced-order model for limit cycle oscillation prediction of nonlinear aeroelastic system, Math. Prob. Eng., 10.1155/2012/152123 · DOI
- Iuliano, 2013, Proper orthogonal decomposition, surrogate Modelling and evolutionary optimization in aerodynamic design, J. Comput. Fluids, 84, 327, 10.1016/j.compfluid.2013.06.007 · DOI
- Chinesta, 2011, Recent advances and new challenges in the use of the proper generalized decomposition for solving multidimensional models, J. Fluids Eng., 18, 395
- Amsallem, 2008, Interpolation method for adapting reduced-order models and application to aeroelasticity, AIAA J., 46, 1803, 10.2514/1.35374 · DOI
- Amsallem, 2012, Nonlinear model order reduction based on local reduced-order bases, Int. J. Numer. Methods Eng., 92, 891, 10.1002/nme.4371 · DOI
- Wirtz, 2014, A posteriori error estimation for DEIM reduced nonlinear dynamical systems, SIAM J. Sci. Comput., 36, A311, 10.1137/120899042 · DOI
- Zhong-Hua Han, Stefan Görtz and Ralf Zimmermann, On improving efficiency and accuracy of variable-fidelity surrogate modeling in aero-data for loads context. CEAS 2009 European Air and Space Conference, Manchester U. K., 26–29 Oct. 2009.
- Craig, 1998, Constructing partial prior specifications for models of complex physical systems, Appl. Stat., 47, 37
- Zimmermann, 2012, Gradient-enhanced surrogate modeling based on proper orthogonal decomposition, Struct. Multidiscip. Optim., 237, 403
- Laurenceau, 2010, Comparison of gradient-based and gradient-enhanced response-surface-based optimizers, AIAA J., 48, 981, 10.2514/1.45331 · DOI
- Han, 2010, Towards efficient high-dimensional aerodynamic shape optimization: surrogate modeling via gradient-enhanced Kriging, vol. 1
- Voutchkov, 2010, vol. 7, 155
- James Parr, C. M. E. Holden, A. I. J. Forrester and A. J. Keane, Review of efficient surrogate infill sampling criteria with constraint handling. 2nd International Conference on Engineering Optimization, 1–10, Portugal, 06-10 Sep 2011.
- Huang, 2013, Research on multi-fidelity aerodynamic optimization methods, Chin. J. Aeronaut., 26, 279, 10.1016/j.cja.2013.02.004 · DOI
- Zahr, 2015, Progressive construction of a parametric reduced-order model for PDE-constrained optimization, Int. J. Numer. Methods Eng., 102, 1111, 10.1002/nme.4770 · DOI
- Allaire, 2010, Surrogate modeling for uncertainty assessment with application to aviation environmental system models, AIAA J., 48, 1791, 10.2514/1.J050247 · DOI
Cited by
Sorted by citations
Items 201–300 of 310
Sogunuru, A., Varughese, S., Niranjanappa, A., & Hemachandra Reddy, K. (2022) · Defence Science Journal · doi:10.14429/dsj.72.17883 · Cited by 3
Expensive Inequality Constraints Handling Methods Suitable for Dynamic Surrogate-based Optimization
Li, C., Fang, H., & Gong, C. (2019) · IEEE Congress on Evolutionary Computation (CEC) · doi:10.1109/cec.2019.8790253 · Cited by 3
“Researchers have delivered a great deal of fruitful results [5,6] in many aspects, such as surrogate modeling, design of experiment (DoE), refinement strategies, and so on.”
BackgroundSurrogate Model-Based Rapid optimization for the Deployment of Combat System of Systems
Ge, B., Xia, B., Yang, K., Zhao, Q., Dou, Y., & Xiang, Z. (2020) · IEEE International Systems Conference (SysCon) · doi:10.1109/syscon47679.2020.9275874 · Cited by 3
“When facing complicated and black-box optimization problem, these traditional methods tend to be inapplicable or inefficient [4].”
MethodHosnifam, S., Mahini, M. R., & Cocchetti, G. (2023) · Meccanica · doi:10.1007/s11012-023-01659-0 · Cited by 2
“[50, 51]), but the choice of the optimal surrogate model requires a specific campaign (see e.”
BackgroundKaneko, H. (2025) · Industrial & Engineering Chemistry Research · doi:10.1021/acs.iecr.4c03669 · Cited by 2
On deep-learning-based closures for algebraic surrogate models of turbulent flows
Eiximeno, B., Sanchís-Agudo, M., Miró, A., Rodriguez, I., Vinuesa, R., & Lehmkuhl, O. (2025) · Journal of Fluid Mechanics · doi:10.1017/jfm.2025.10610 · Cited by 2
Experimental study on the underwater propulsion performance of bionic flexible flapping fins
Zhou, M., Wu, Z., & Yang, C. (2025) · Ocean Engineering · doi:10.1016/j.oceaneng.2025.123146 · Cited by 2
Manifold-Preserving Guided Aerodynamic Modeling for Heterogeneous Data
Liu, Y., Liu, Z.-T., Guo, S.-Q., Nie, H., Liu, W., Zhang, C.-A., & Yan, X. (2025) · AIAA Journal · doi:10.2514/1.j065256 · Cited by 2
Liu, B., Tan, J., Lyu, H., Zhang, Z., Liu, Z., & Huang, H. L. (2025) · Aerospace Science and Technology · doi:10.1016/j.ast.2025.111299 · Cited by 2
Study on the Design Methodology of Turbine Profiles Operating Within Wide-Inflow-Angle Ranges
Zhang, R., Zhang, W., & Lei, C. (2025) · Journal of Propulsion and Power · doi:10.2514/1.b39619 · Cited by 2
Liu, Y., Yang, Y., Jin, J., Xiao, Z., Wan, J., & Long, X. (2025) · Process Safety and Environmental Protection · doi:10.1016/j.psep.2025.108281 · Cited by 2
Toward a GPU-enabled billionaire SVD in pyLOM
Miró, A., Eiximeno, B., Gasparino, L., Kutz, N., Rodríguez, I. M., & Lehmkuhl, O. (2026) · Acta Mechanica · doi:10.1007/s00707-025-04621-1 · Cited by 2
Interval model calibration with response-consistent supervised learning network
Zhao, Y., Yun, Q., Bi, S., Wang, X., & Beer, M. (2026) · Mechanical Systems and Signal Processing · doi:10.1016/j.ymssp.2026.113942 · Cited by 2
Development of neural network-based surrogate models in geotechnics: a state-of- the-art review
Cerek, K., Dao, D. A., Hadjiloo, E., & Grabe, J. (2026) · Machine Learning and Data Science in Geotechnics · doi:10.1108/mlag-04-2025-0011 · Cited by 2
Li, C., & Dong, H. (2022) · Engineering Computations · doi:10.1108/ec-08-2021-0456 · Cited by 2
Design Space Reduction using Multi-Fidelity Model-Based Active Subspaces
Mufti, B., Perron, C., Gautier, R. H., & Mavris, D. N. (2023) · AIAA AVIATION Forum · doi:10.2514/6.2023-3592 · Cited by 2
Handayani, P. A., Devi, A. L., & Ganisha, N. A. (2023) · IOP Conference Series Earth and Environmental Science · doi:10.1088/1755-1315/1203/1/012002 · Cited by 5
“However, to find out an optimum process that is influenced by several variables, a lot of experimental data is needed, which takes a long time and costs a lot of money [24].”
BackgroundA new approach for data-driven surrogate modelling applied in highly nonlinear engineering functions
Parnianifard, A., Sharma, A., & Chaudhary, S. (2024) · Journal of Statistical Computation and Simulation · doi:10.1080/00949655.2024.2439488 · Cited by 2
“Some of the relative applications of surrogates in practical engineering problems can be featured in antenna design [34–37], robotics [38], optimal control [39,40], wireless communication [41,42], supply chain management [39,43], aircraft [32,44,45], and robust design under uncertainty [46–48].”
Data-driven modeling for rapid prediction of aerodynamic noise directivity of flow over a cylinder
Jin, Y. H., Liao, F., & Cai, J. (2025) · Applied Mathematical Modelling · doi:10.1016/j.apm.2025.115937 · Cited by 2
Implementation and Assessment of Machine Learning Methods for Multidisciplinary Aerospace Problems
Kilic, D., & Nikbay, M. (2025) · AIAA SciTech Forum · doi:10.2514/6.2025-0492 · Cited by 3
A machine learning approach to modelling temperature-dependent cyclic behaviour
Sverdrup, F., Pellegrino, A., Tagarielli, V. L., & Tasdemir, B. (2025) · Materials Today Communications · doi:10.1016/j.mtcomm.2025.112369 · Cited by 2
Xu, X., Fang, X., & Yu, X. (2025) · Aerospace · doi:10.3390/aerospace12070567 · Cited by 2
Enderle, B., Rauch, B., Grimm, F., Eckel, G., & Aigner, M. (2023) · Flow Turbulence and Combustion · doi:10.1007/s10494-023-00426-1 · Cited by 2
“Among the various models proposed in the literature (Forrester and Keane 2008; Yondo and Andrés 2018), Polynomial Chaos Expansion (PCE) in combination with sparse quadrature approaches (Le Maître and Knio 2010) have drawn increasing attention for the use in UQ (Najm 2009; Sheen and Wang 2011; de Souza and Colaço 2014).”
BackgroundAutoEmulate: A Python package for semi-automated emulation
Stoffel, M. A., Li, B. M., Westerling, K., Arana, S., Balmus, M., Daub, E. G., & Niederer, S. (2025) · The Journal of Open Source Software · doi:10.21105/joss.07626 · Cited by 2
“Emulation is becoming increasingly widespread, ranging from engineering (Yondo et al., 2018), architecture (Westermann & Evins, 2019), biomedical (Strocchi et al., 2023) and climate science (Bounceur et al., 2015), to agent-based models (Angione et al., 2022).”
Blade planform improvement and airfoil shape optimization of helicopters in hover flight
Shahmiri, F., & Badihi, M. E. (2020) · Journal of the Brazilian Society of Mechanical Sciences and Engineering · doi:10.1007/s40430-020-02499-9 · Cited by 1
Geng, J., Qi, H., Li, J., & Wang, X. (2024) · Journal of Engineering for Gas Turbines and Power · doi:10.1115/1.4065994 · Cited by 1
A non-uniform multi-point incremental Kriging facing with discrete response surfaces
Wang, S., Lu, H., & Zhang, Y. (2024) · Applied Soft Computing · doi:10.1016/j.asoc.2024.112397 · Cited by 1
Optimal design for a gravity-balanced compliant mechanism
Chau, N. L., Vo, H. X., & Dao, T.-P. (2024) · International Journal on Interactive Design and Manufacturing (IJIDeM) · doi:10.1007/s12008-024-02190-6 · Cited by 1
“Design of experiments (DOE) methods are utilized to determine a series of enough experiments in numerical analysis or physical test [16].”
Chimauriya, H. R., Biswas, N., Gajurel, A., & Puppala, A. J. (2025) · Geotechnical Frontiers · doi:10.1061/9780784485989.003 · Cited by 1
Lucarelli, L. C., Blal, N., Platzer, A., Gravouil, A., & Iampietro, D. (2025) · Finite Elements in Analysis and Design · doi:10.1016/j.finel.2025.104386 · Cited by 1
Chimauriya, H. R., Biswas, N., Puppala, A. J., & Gajurel, A. (2025) · Canadian Geotechnical Journal · doi:10.1139/cgj-2025-0118 · Cited by 1
Assessment of Oscillating Wings to Deliver Air Mass Flow Under Power and Thrust Constraints
Özyılmaz, E. B., & Kaya, M. (2025) · Aerospace · doi:10.3390/aerospace12080740 · Cited by 1
“Through the integration of data-driven insights, machine learning methods like artificial neural networks (ANNs) or support vector regression (SVR) offer reliable means for prediction, optimization, and design enhancement [24].”
Yang, Y., López, A. R., Tsiampousi, A., & Taborda, D. M. G. (2026) · Data-Centric Engineering · doi:10.1017/dce.2025.10036 · Cited by 1
“…large number of simulations or real-time decision-making (Jones et al., 1998; Jones, 2001), e.g., civil engineering (Asher et al., 2015; Nini ć et al., 2017; Qi and Fourie, 2018; Cao et al., 2020), aerospace engineering (Yondo et al., 2018), and chemical engineering (McBride and Sundmacher, 2019).”
A novel dual-branch graph-based reconstruction framework of thermal fields for orbital satellites
Li, Q., Xu, W., Lv, N., Zhang, S., Zhang, Y., Zhao, X., Xia, Y., & Li, X. (2026) · Aerospace Science and Technology · doi:10.1016/j.ast.2026.112513 · Cited by 1
Cao, W., Wang, B., Chen, J., Li, X., Dong, T., Ma, Q., & Li, W. (2026) · Applied Energy · doi:10.1016/j.apenergy.2026.128057 · Cited by 1
Critical Evaluation into the practical utility of the Design of Experiments
Sharma, M. J., & Sharma, S. (2021) · Engineering Management in Production and Services · doi:10.2478/emj-2021-0021 · Cited by 1
“Aviation Space and Environmental Medicine, 67, 235-242.”
MethodMachine Learning based Surrogate Assisted Multi-Objective Optimization of Continuous Casting Process
Inapakurthi, R. K., & Mitra, K. (2021) · Indian Control Conference · doi:10.1109/icc54714.2021.9703180 · Cited by 1
Robustness Analysis on the Aerothermal Performance of Turbine Blade Squealer Tip
Huang, M. N., Li, Z., & Li, J. (2022) · Journal of Engineering for Gas Turbines and Power · doi:10.1115/1.4054377 · Cited by 1
Research of a novel aerodynamic evaluation method for fixed-wing UAV
Wu, Y., Liu, D., Wang, T., & Zhao, A. (2023) · Journal of Physics Conference Series · doi:10.1088/1742-6596/2633/1/012001 · Cited by 1
A Novel Constrained Latin Hypercube Sampling for Electric Machine
Li, J., Tan, N. M. L., Xu, Z., & Fu, W. N. (2023) · IEEE Industrial Electronics and Applications Conference (IEACon) · doi:10.1109/ieacon57683.2023.10370299 · Cited by 1
“These methods primarily take into consideration the randomness and nonrepeatability encountered in field experiments or computer simulations [11].”
MethodPDOPT: A Python library for Probabilistic Design space exploration and OPTimisation
Spinelli, A., & Kipouros, T. (2024) · The Journal of Open Source Software · doi:10.21105/joss.06110 · Cited by 1
“In the computational engineering field, quasi-random sampling is preferred, with Latin Hypercube sampling and Sobol sequences being most used (Yondo et al., 2018).”
MethodSequential sampling for functional estimation via Sieve
Benevento, A., Ahadi, P., Gupta, S., Pacella, M., & Paynabar, K. (2024) · Quality and Reliability Engineering International · doi:10.1002/qre.3557 · Cited by 1
Hou, Z., Lin, Y., Liu, T., & Lu, W. (2024) · Environmental Science and Pollution Research · doi:10.1007/s11356-024-33405-8 · Cited by 1
“…learning methods, which are employed as pattern recognition tools to replace the numerical model and avoid com-putation-expensive iterations (Yondo et al. 2018; Luo et al. 2020; Jiang et al. 2021), i.e., intelligent surrogate models are required, while maintaining a high computational…”
Márquez-Grajales, A., Mezura‐Montes, E., Acosta‐Mesa, H., & Salas-Martínez, F. (2024) · Mathematical and Computational Applications · doi:10.3390/mca29050078 · Cited by 1
“The solutions were randomly initialized within the search space following a uniform distribution [21,63–65].”
Compression resistance of horsetail-inspired porous thin-walled structures
Xie, B., Xie, X., Yang, Y., Han, L., Yan, F., & Lu, Z. (2025) · Proceedings of the Institution of Mechanical Engineers Part L Journal of Materials Design and Applications · doi:10.1177/14644207251329490 · Cited by 1
“31,32 Using the BBD experimental design and simulation data, 33 multiple regression fi tting was applied to the HH-type structure, establishing the functional relationship between each response and related factors, as follows: The type HHFH structure was fi tted with multiple regression, as follows:…”
Nakasima-López, S., Nakasima-López, M. O., Estrada, K. F. M., & Salomón, E. B. (2019) · Advances in chemical and materials engineering book series · doi:10.4018/978-1-7998-1518-1.ch012 · Cited by 1
Wu, Y., Long, T., Shi, R., & Wang, G. G. (2019) · AIAA AVIATION Forum · doi:10.2514/6.2019-3667 · Cited by 1
RetractedNumber of DoE Required for Estimating Different Quality Surrogate
Yin, L., Wang, S., Lv, L., Song, X., Guo, Z., & Sun, W. F. (2021) · International Journal of Computational Methods · doi:10.1142/s021987622141019x · Cited by 1
Koziel, S. M., & Pietrenko‐Dabrowska, A. (2020) · Springer eBooks · doi:10.1007/978-3-030-38926-0_1 · Cited by 1
Rubio-Clemente, A., Aguilar, J., & Chica, E. (2020) · Renewable Energy and Power Quality Journal · doi:10.24084/repqj18.258 · Cited by 1
"Review on Surrogate-Based Global Optimization with Biomedical Applications"
Haridy, A. (2023) · Biomedical Journal of Scientific & Technical Research · doi:10.26717/bjstr.2023.53.008409 · Cited by 1
Chang, Y., Wang, X., Zhang, L., Li, Y., Mak, S., Wu, C. F. J., & Yang, V. (2021) · arXiv (Cornell University) · doi:10.48550/arxiv.2101.08893 · Cited by 1
“The results are consistent with the previous finding that the CPOD method can accurately capture major performance metrics, such as time-averaged liquid film thickness and spreading angle, but not detailed flow dynamics [10,11].”
BackgroundResultHao, Z., Zhang, C., & Lapkin, A. A. (2021) · doi:10.33774/chemrxiv-2021-v88c7 · Cited by 1
Non-intrusive reduced order modelling for aerodynamic applications
Balla, K. (2021) · doi:10.23889/suthesis.58705 · Cited by 1
Park, J., & Kim, H. (2023) · SSRN Electronic Journal · doi:10.2139/ssrn.4480466 · Cited by 1
Pylom: A Hpc Open Source Reduced Order Model Suite for Fluid Dynamics ApplicationsPreprint
Eiximeno, B., Miró, A., Begiashvili, B., Valero, E., Rodriguez, I., & Lehmkuhl, O. (2024) · SSRN Electronic Journal · doi:10.2139/ssrn.4856967 · Cited by 1
Self-citationA hybrid analytical-numerical algorithm for determining the neuronal current via EEGPreprint
Hashemzadeh, P., FOKAS, A. S., & Schönlieb, C. (2019) · arXiv (Cornell University) · doi:10.48550/arxiv.1906.01403
“Regression Model of us(r, τ , τ̂ ) For A Realistic Head Model Regression models constructed using data generated by PDE solvers are referred to as surrogate models [18, 19, 20, 21, 22, 23].”
MethodAdaptive Experimental Design for Aerodynamic Modeling with Hard-to-Change Factors
Choi, U., Sung, T., & Ahn, J. (2020) · Journal of Aerospace Information Systems · doi:10.2514/1.i010813
Parnianifard, A., Wuttisittikulkij, L., Zemouche, A., & Phanomchoeng, G. (2020) · doi:10.21203/rs.3.rs-52777/v1
“However, several studies have systematically illustrated the applications of surrogate-based optimization algorithms [36], [37], [41]– [43].”
BackgroundA novel ISLE-ESE method for mixed-variable experiment design
Yang, J., Wu, Z., Wang, W., li, J., Zhang, W. H., Jinhua, S., Zhao, H. L., Wen, Q., & Zhen, X. (2021) · IOP Conference Series Materials Science and Engineering · doi:10.1088/1757-899x/1043/2/022043
“, the input based space-filling design and output based design([6]).”
BackgroundWakimoto, K., Chiba, K., Kato, H., & Nakakita, K. (2021) · Aerospace · doi:10.3390/aerospace8080217
“Furthermore, dimensionality reduction for aerodynamic data acquired by WTT [4] must work better when the data set is generated consecutively/automatically rather than discrete/manually, regardless of any data reduction methods.”
MethodParnianifard, A., Mumtaz, S., Chaudhary, S., Imran, M. A., & Wuttisittikulkij, L. (2021) · Research Square · doi:10.21203/rs.3.rs-976342/v1
“To handle this, Kriging surrogate (also known as the Gaussian process) has been applied for different types of engineering design problems [23]–[25].”
MethodKnowledge-Driven Adaptive Sequential Modeling and Prediction of Aerodynamic Characteristics
Pu, X., Hao, J., Zhang, F., He, S., & Long, Y. (2022) · Mechanisms and machine science · doi:10.1007/978-981-16-7381-8_91
Tan, J., Chen, H., Ye, X., & Lin, Y. (2022) · Energies · doi:10.3390/en15134826
Augmenting covariance estimation for ensemble-based data assimilation in multiple-query scenarios
Ilersich, A. F., Schau, K. A., Oefelein, J. C., Steinberg, A. M., & Yano, M. (2022) · Combustion Theory and Modelling · doi:10.1080/13647830.2022.2105259
“This family may contain many different but closely related configurations [24], or it may contain a single configuration undergoing relatively slow changes in operating conditions, as in the digital twin configuration [3].”
BackgroundLeal, G. D. S., Romão, E. L., dos Reis, D. L. D. P. E., Balestrassi, P. P., & de Paiva, A. P. (2022) · Production · doi:10.1590/0103-6513.20210119
“According to (Yondo et al., 2018), industrial experiments have been focusing mainly on 2-levels and 3-levels designs, resulting in 2 and 3 experiments, respectively.”
BackgroundPietrenko‐Dabrowska, A., & Koziel, S. M. (2023) · Springer eBooks · doi:10.1007/978-3-031-43845-5_1
Wang, B., Cao, W., Dong, T., Zhen, X., Liu, J., Sun, Y., & Zhou, L. (2023) · International Conference on Smart Grid and Smart Cities (ICSGSC) · doi:10.1109/icsgsc59580.2023.10319219
“In order to address this problem, the surrogate model was developed[6].”
BackgroundMethodInfluentialAdaptive Elliptic Basis Function Model Construction Strategy Based on Particle Swarm Optimization
Lin, S., Rong, B., & Yang, S. (2024) · Lecture notes in mechanical engineering · doi:10.1007/978-981-99-8048-2_172
Active Learning Enhanced Surrogate Modeling of Jet Engines in JuliaSim
Abdelrehim, A., Gandhi, D., Yalburgi, S., Bharambe, A., Anantharaman, R., & Rackauckas, C. (2025) · AIAA SciTech Forum · doi:10.2514/6.2025-2323
SMT-EX: An Explainable Surrogate Modeling Toolbox for Mixed-Variables Design Exploration
Robani, M. D., Saves, P. M. V., Palar, P. S., Zuhal, L., & Morlier, J. (2025) · AIAA SCITECH 2025 Forum · doi:10.2514/6.2025-0777 · Cited by 5
“Surrogate models are commonly employed to efficiently address multi-query tasks [2].”
Moussaoui, Z., karafi, Y., & Majd, B. A. E. (2025) · SSRN Electronic Journal · doi:10.2139/ssrn.5159267
Yang, Y., & Sato, Y. (2025) · Lecture notes in computer science · doi:10.1007/978-981-96-3538-2_12
Sparse Sampling and Fusion of Multi-Fidelity Aerodynamic Heating Data
Nie, Y., Yang, C., Wei, M., Jiang, X., & Ma, X. (2024) · International Congress on Image and Signal Processing (CISP) · doi:10.1109/cisp-bmei64163.2024.10906155
Miao, X., & Liu, C. (2025) · Nonlinear Dynamics · doi:10.1007/s11071-025-11524-2 · Cited by 1
Ding, Y., Jin, D., Zhang, J., & Guo, H. (2025) · Journal of Aerospace Engineering · doi:10.1061/jaeeez.aseng-6156
Xia, Z., Yin, H., Wang, X., & Fu, J. (2025) · Physics of Fluids · doi:10.1063/5.0285808
Sánchez, L. F., Vallerio, M., & Manenti, F. (2025) · Engineering Reports · doi:10.1002/eng2.70422
“The maxmin LHS is a space-filling DoE based on the LHS, which aims to improve the spatial distribution of samples [8].”
InfluentialYou, D., Zheng, S., Li, F., & Luo, X. (2025) · Journal of Manufacturing and Materials Processing · doi:10.3390/jmmp9110358
“Yondo et al. compared the kriging and response surface models and found that, although the high-order response surface is applicable to highly nonlinear problems, it needs a large training set and thus has an unstable performance [19].”
MLPA-GASA: A Novel Surrogate-Assisted Hybrid Algorithm for Wind Farm Layout Optimization
Shang, W., Gong, L., Liu, X., Liu, M., & Xiang, X. (2025) · Lecture notes in electrical engineering · doi:10.1007/978-981-95-1252-2_22
Efficient Aerodynamic Surrogate Modeling of Switchblade UAVs for Digital Twin
Lyu, H., & Cao, R. (2025) · International Conference on Robotics, Control and Automation Engineering (RCAE) · doi:10.1109/rcae66389.2025.11355242
“Sampling the design space, that is, selecting a good set of data points, is crucial for simulation, with the main goal of obtaining the maximum amount of information from a limited number of samples [6].”
Multi-fidelity surrogate modeling with low-fidelity auxiliary sampling for fluid flow prediction
Yang, C., Hai, C., Tang, H., & Mei, L. (2026) · Physics of Fluids · doi:10.1063/5.0312674
A multi-strategy improved marine predator algorithm for large-scale optimization
Liu, B., Ren, W., Li, H., Liang, Y., Li, J., & Gao, L. (2026) · International Conference on Communication Networks and Machine Learning (CNML) · doi:10.1109/cnml68938.2026.11453131
“For instance, in aircraft design[1], it is essential to optimize dimensions and configurations to enhance performance, while in robotic path planning and control [2], finding optimal trajectories is crucial.”
Data assimilation with reduced basis and noisy measurement : Applications to nuclear reactor cores
Gong, H. (2018) · doi:10.70675/0ae0fc95z5f38z4025zad3azd5d96ad9545a
“A favoured application of ROM is in aerodynamic analyses [217, 212].”
MethodWang, B., Zhong, L., Meng, Z., Wu, Y., & Shu, L. (2026) · Ocean Engineering · doi:10.1016/j.oceaneng.2026.125449
Projection-based model reduction using Pressio: application to hypersonic aerothermodynamics
Rizzi, F., Parish, E., Blonigan, P., Tencer, J. T., Wentland, C. R., Kurzawski, A. J., Heyningen, R. L. V., Schilly, C., & Brunini, V. (2026) · Structural and Multidisciplinary Optimization · doi:10.1007/s00158-026-04300-2
“Typical many-query problems require thousands of model evaluations to characterize the effect of uncertainties in parameters and operating conditions on the system response (Yondo et al. 2018; Kelley 1999).”
Jalal, A., Hassan, W. U., Akram, U., Buzal, M. Z., Malik, M. A. I., Asim, A., Asghar, H., Jamil, S. R., & Usman, M. (2026) · Next Energy · doi:10.1016/j.nxener.2026.100652
Wang, Y., Baoqing, Y. A. N. G., Li, P., Wang, S., & Ma, D. J. (2026) · Applied Mathematical Modelling · doi:10.1016/j.apm.2026.117047
Surrogate-Assisted Optimization of Hypersonic Gliding Vehicle for Range Extension in Re-entry Flight
Yixing, S., Shi, R., & Tai, X. (2026) · Mechanisms and machine science · doi:10.1007/978-981-95-7342-4_35
Liu, J., Qian, W., Zhao, Y., Hu, X., & Ai, X. (2026) · Aerospace Science and Technology · doi:10.1016/j.ast.2026.112709
A Preliminary Analysis of a Physics-Informed Neural Network for the Forward Problem in EEG
FOKAS, A. S., Aghaei, A. A., & Hashemzadeh, P. (2026) · BioMedInformatics · doi:10.3390/biomedinformatics6040042
Industrial CFD and Fluid Modeling in Engineering: Third Edition
Vanna, F. D. (2026) · Fluids · doi:10.3390/fluids11070174
“The aerodynamics are resolved with three-dimensional RANS computations of the NREL Phase VI rotor using the transition SST k – ω model [36,37], and the deflector geometry is optimized through a Box–Behnken response-surface model whose quadratic fit attains an R 2 of 0.98 [3,38].”
InfluentialReduced Multifidelity Low-Sonic-Boom Design for Supersonic Transport by Manifold Alignment
Xiao, L., Chao, S., Zhu, Z., Hongyang, L., Yu, T., & Tao, T. (2026) · Journal of Aircraft · doi:10.2514/1.c039004
Benson, T., Kim, H., Seo, J., & Hassan, Y. A. (2026) · Nuclear Engineering and Design · doi:10.1016/j.nucengdes.2026.115143
Metadata
- Authors
- Yondo, R., Andrés, E., & Valero, E.
- Affiliations
- Universidad Politécnica de Madrid (ES)
- Ingeniería de Sistemas para la Defensa de España (ES)
- Corresponding author
- Yondo, Raul
- Venue
- Progress in Aerospace Sciences
- Publisher
- Elsevier BV
- Published
- 2018-01
- Volume
- 96
- Pages
- 23-61
- ISSN
- 0376-0421 (ISSN-L)
- OpenAlex
- W2776493547
- Cited by
- 311
- References
- 548
- Citations by year
- 2026: 29 · 2025: 50 · 2024: 44 · 2023: 32 · 2022: 49 · 2021: 41 · 2020: 39 · 2019: 26 · 2018: 1
- FWCI
- 13.56
- Type
- journal article
- Language
- en
- Open access
- closed
- Locations
- Progress in Aerospace Sciences (publishedVersion)
- Funders
- European Commission Seventh Framework Programme (FP7-PEOPLE-2013-ITN, 608087)
- Topics
- Physical Sciences › Computer Science › Computational Theory and Mathematics › Advanced Multi-Objective Optimization Algorithms
- Physical Sciences › Engineering › Computational Mechanics › Probabilistic and Robust Engineering Design
- Physical Sciences › Engineering › Computational Mechanics › Computational Fluid Dynamics and Aerodynamics
- Keywords
- surrogate models, aircraft aerodynamic design, surrogate-based optimization, experimental design, sampling strategy, dimensionality reduction, sensitivity analysis, uncertainty quantification, multi-fidelity modeling, civil transport aircraft, computational complexity reduction
About these checks
Registry, retraction, Cites and statistics results are computed, not judged, with one exception: a printed reference that no index lists is read once by a model before it counts as a citation error. Claims are extracted by a model and kept only when their quote appears verbatim in the text; each cited source is then checked, with a model’s help, for whether it says what the claim relies on. Those verdicts can be wrong — read the claim’s quote and the cited source before relying on one.
Statistics and arithmetic are recomputed, not judged.
Confidence bands are shown only for fields calibrated on our annotated test set. None is calibrated yet, so no band is shown.
What counts as a claim ›How we measure confidence ›How we check this ›
Are you an author, or do you see a problem with this page? Request a review