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international journal of advanced design and manufacturing technology
سال:2023 - دوره:16 - شماره:2
active control of shimmy vibration in aircraft nose landing gear using fuzzy and narma-l2 controllers
- صفحه:55-64
analysis of fgm cylindrical shell under impact loading of explosion
- صفحه:65-76
finite element analysis of the impact behavior of sandwich panels with nanocomposite face sheet (epoxy/ fiberglass/nanosilica)
- صفحه:25-33
frequency analysis of ring-stiffened composite cylindrical shell using experimental, analytical and finite element methods
- صفحه:1-11
improvement analysis of response between jacket platforms and sea waves using the vibration dampers
- صفحه:103-111
investigating the effect of process parameters on reducing the peeling stress in adhesive joints of composite materials
- صفحه:77-90
minimum stiffness and optimal position of an intermediate elastic support to maximize the fundamental frequency of a vibrating timoshenko beam using finite element method and multi-objective genetic algorithm
- صفحه:13-23
study on the thermophysical properties of hybrid nanofluid based on aircraft de/anti-icing fluid at low temperatures
- صفحه:91-102
vibration analysis of rotating disk carrying annular concentrated masses in turbo-pump system
- صفحه:45-53
vibration behavior of the planetary gear system by considering the fixed output
- صفحه:35-43
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