04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
RATIONAL DETERMINATION OF WING JIG SHAPE OF A LONG-RANGE AIRCRAFT WITH TRANSONIC CRUISE REGIME
A.V. Bezuevsky¹, A.V. Grigorev¹; ¹Central Aerohydrodynamic Institute (TsAGI), Russia
The paper presents the developed iterative procedure for calculations of the wing jig shape for long range aircraft. The results of parametric study of structural mass and fuel consumption in dependence on the jig shape are presented. The recommendations on the rational choice of the wing jig shape are formulated.