Browsing Acta Polytechnica. 2017, vol. 57 by Subject "aerodynamics, panel method, finite element method, wing load"

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    • AERODYNAMIC LOAD OF AN AIRCRAFT WITH A HIGHLY ELASTIC WING 

      Author: Schoř , Pavel
      (České vysoké učení technické v PrazeCzech Technical University in Prague, 2017)
      In this article, a method for calculation of air loads of an aircraft with an elastic wing is presented. The method can predict a redistribution of air loads when the elastic wing deforms. Unlike the traditional Euler or ...