An efficient method for predicting zero-lift or boundary-layer drag including aeroelastic effects for the design environment

Publisher： Cambridge University Press

E-ISSN： 2059-6464|119|1221|1451-1460

ISSN： 0001-9240

Source： The Aeronautical Journal, Vol.119, Iss.1221, 2015-11, pp. : 1451-1460

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract

Related content

Effects of boundary-layer bleeding on unstart oscillatory flow of hypersonic inlets

By  

The Aeronautical Journal, Vol. 114, Iss. 1157, 2010-07 ,pp. : 445-450

Cambridge University Press

Access to resources Recommend Favorite

Design of morphing winglets with the inclusion of nonlinear aeroelastic effects

By  

The Aeronautical Journal, Vol. 115, Iss. 1174, 2011-12 ,pp. : 713-728

Cambridge University Press

Access to resources Recommend Favorite

The solution of the Falkner-Skan equation arising in the modelling of boundary-layer problems via variational iteration method

By Dehghan Mehdi   Tatari Mehdi   Azizi Asma  

International Journal of Numerical Methods for Heat & Fluid Flow, Vol. 21, Iss. 2, 2011-03 ,pp. : 136-149

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Effects of viscous dissipation and Newtonian heating on boundary-layer flow of nanofluids over a flat plate

By Makinde Oluwole Daniel  

International Journal of Numerical Methods for Heat & Fluid Flow, Vol. 23, Iss. 8, 2013-10 ,pp. : 1291-1303

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Modelling the aeroelastic response and flight dynamics of a hingeless rotor helicopter including the effects of rotor-fuselage aerodynamic interaction

By  

The Aeronautical Journal, Vol. 119, Iss. 1214, 2015-04 ,pp. : 433-478

Cambridge University Press

Access to resources Recommend Favorite