1. Campbell RL, Lynde MN. Building a practical natural laminar flow design capability. 35th AIAA applied aerodynamics conference. Reston: AIAA; 2017. p. 1–21.
2. Multi-objective optimisation of short nacelles for high bypass ratio engines;Tejero;Aerosp Sci Technol,2019
3. Fang XM, Zhang YF, Chen HX. Transonic nacelle aerodynamic optimization based on hybrid genetic algorithm. 34th AIAA applied aerodynamics conference. Reston: AIAA; 2016. p. 13-7.
4. Vermeersch O, Bouteiller X. Numerical study of laminar nacelles: Natural and hybrid laminar flow designs. Int J Eng Syst Model Simul 48 2014; 6(3-4):191-204.
5. Lamb M, Aabeyounis W, Patterson Jr JC. Nacelle/pylon/wing integration on a transport model with a natural laminar flow nacelle. Washington, D.C.: NASA; 1985. Report No.: NASA Technical Paper 2439.