25th Congress of International Council of the Aeronautical Sciences, 3 - 8 September 2006, Hamburg, Germany
Paper ICAS 2006-10.5.3

MATRIX FORMULATION FOR CALCULATIONS OF WING LOADING DISTRIBUTION

A. Pistek
Brno University of Technology, Czech Republic

Keywords: aircraft, load distribution, matrix, automation

The paper describes the application of matrix formulation for calculation of loading of airplane. The most work – difficulty and time-consuming computations are done only once and the matrixes include mainly simple geometrical date.The method, was successfully applied in the software SAVLE, used during the development of several Czech airplanes

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