Aerodynamic Optimization of an Over-the-Wing-Nacelle-Mount Configuration

Article English OPEN
Daisuke Sasaki; Kazuhiro Nakahashi;

An over-the-wing-nacelle-mount airplane configuration is known to prevent the noise propagation from jet engines toward ground. However, the configuration is assumed to have low aerodynamic efficiency due to the aerodynamic interference effect between a wing and a nacel... View more
  • References (15)
    15 references, page 1 of 2

    Fujino, M., Kawamura, Y.. Wave-drag characteristics of an over-the-wing nacelle business-jet configuration. Journal of Aircraft. 2003; 40 (6): 1177-1184

    Ricouard, J., Davy, R., Loheac, P., Moore, A., Piccin, O.. ROSAS wind tunnel test campaign dedicated to unconventional aircraft concepts study. : 783-792

    Sasaki, D., Obayashi, S.. Efficient search for trade-offs by adaptive range multi-objective genetic algorithms. Journal of Aerospace Computing, Information and Communication. 2005; 2 (1): 44-64

    Sunago, M., Sasaki, D., Takenaka, K., Nakahashi, K.. Multipoint optimization of a short-range quiet passenger aircraft. Journal of Aircraft. 2009; 46 (3): 1070-1074

    Jeong, S., Minemura, Y., Obayashi, S.. Optimization of combustion chamber for diesel engine using kriging model. Journal of Fluid Science and Technology. 2006; 1: 138-146

    Jeong, S., Murayama, M., Yamamoto, K.. Efficient optimization design method using kriging model. Journal of Aircraft. 2005; 42 (2): 413-420

    McKay, M. D., Beckman, R. J., Conover, W. J.. A comparison of three methods for selecting values of input variables in the analysis of output from a computer code. Technometrics. 1979; 21 (2): 239-245

    Sobieczky, H.. Parametric airfoils and wings. Notes on Numerical Fluid Mechanics. 1998: 71-88

    Ito, Y., Nakahashi, K.. Surface triangulation for polygonal models based on CAD data. International Journal for Numerical Methods in Fluids. 2002; 39 (1): 75-96

  • Metrics
Share - Bookmark