EXPERIMENTAL AND FINITE ELEMENT ANALYSIS FOR COMPOSITE AIRCRAFT STRUCTURES.

Experimental modal testing of a honeycomb sandwich plate

An Experimental Testing of an UAV Composite Wing Structure

SOME ASPECTS OF AN EXPERIMENTAL INVESTIGATION ON COMPOSITE AEROBATIC AIRCRAFT STRUCTURE.

Flexural investigation of a composite trussed-beam for aerospace shelters using numerical modelling

MODELLING OF VIBRATION DAMPING IN COMPOSITE STRUCTURES

Vibration analysis of composite wing with geometric and material coupling

Mechanical and Dynamic Properties of Hybrid Composite Laminates

Enhanced Mechanical Evaluation of Natural Fiber Composite Sandwich Panels for Aircraft Structures

A MODAL ANALYSIS OF A VIBRATING SANDWICH CANTILEVER BEAM