28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
ANALYTICAL METHOD FOR LIMIT LOAD CAPACITY CALCULATION OF THIN WALLED AIRCRAFT STRUCTURES
Inst. of Aerospace Eng., Brno Univ. of Technology, Czech Republic
Keywords: limiting load, stress analyses, buckling and post buckling behavior
The paper describe the methods for limit load capacity calculation of thin walled aircraft structures by the all possible forms of buckling and failures under loading. Special attention is focused on method so called “gradually increased loading method” - GILM (original method developed by the author of this paper).
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