The effect of aircraft wind modelling on the external store loads is investigated by computing that effect for the external flow field generated by the wing. The application of the panelling /boundary condition method to the perturbation flow field below the wing is first considered; then, the effect of the wing panelling in the leading edge region, where the singularity distributions show large gradients, on the flow field is studied. Both lift and thickness effects are taken into account.
Reference:
Van Den Broek, G. J. 1984. Application of panel methods in external store load calculations. Journal of Aircraft, Vol. 21(7), pp. 537-539.
Van Den Broek, G. (1984). Application of panel methods in external store load calculations. http://hdl.handle.net/10204/2247
Van Den Broek, GJ "Application of panel methods in external store load calculations." (1984) http://hdl.handle.net/10204/2247
Van Den Broek G. Application of panel methods in external store load calculations. 1984; http://hdl.handle.net/10204/2247.
