Publisher
Springer Nature Switzerland
Reference5 articles.
1. Shi Q, Wang H, Cheng H, Cheng F, Wang M (2021) An adaptive sequential sampling strategy-based multi-objective optimization of aerodynamic configuration for a tandem-wing UAV via a surrogate model. IEEE Access 9:164131–164147. https://doi.org/10.1109/ACCESS.2021.3132775
2. Minardo A (2014) The Tandem Wing: Theory, experiments, and practical realisations. Dissertation, Politecnico Di Milano, Milano. https://www.politesi.polimi.it/bitstream/10589/93619/1/2014_07_Minardo.pdf
3. Sutugin LI (1945) Osnovy proektirovaniya samolyotov (Basics of aircraft design). Oborongiz, Moscow
4. Seryoznov AN (ed) (1989) Rukovodstvo dlya konstruktorov letatelnyh apparatov samodeyatelnoy postroyki (Manual for designers of self-made aircraft). Siberian Scientific Research Institute Of Aviation, Novosibirsk
5. Cheng H, Wang H (2018) Prediction of lift coefficient for tandem wing configuration or multiple-lifting-surface system using Prandtl’s lifting-line theory. Int J Aerospace Eng. https://doi.org/10.1155/2018/3104902