Synthesis of the shape of the elastic axis of a closed wing of the aircraft and the study of its stress strain state by the speckle holography method

Features of the stress-strain state of the joined wing of the aircraft. Algorithm for finding the optimal shape of the elastic axis of the wing. We adapt the shape of the aircraft to the flight mode using actuators of alloys with shape memory. Speckle holography is used to clarify the VAT of multiply connected designs.