航空复合材料加筋板剪切稳定性及后屈曲承载性能
Stability and post-buckling carrying capacity of aeronautic composite stiffened panel under shear loading

DOI: 10.13801/j.cnki.fhclxb.20170413.001

Keywords: 复合材料加筋板,剪切,屈曲,后屈曲,理论分析
composite stiffened panel,shear,buckling,post-buckling,theoretical analysis

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