Results 11 to 20 of about 1,252,052 (302)
Virtual testing of post-buckling behaviour of metallic stiffened panel [PDF]
The aim of the project presented in this thesis is to demonstrate a modelling method for predicting the variability in the ultimate load of stiffened panel under axial compression due to manufacturing variability.
Wang, Yang
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Dynamic analysis of an orthotropic viscoelastic cylindrical panel of variable thickness [PDF]
The intensive development of the modern industry is associated with the emergence of a variety of new composite materials. Plates, panels, and shells of variable thickness made of such materials are widely used in engineering and machine building. Modern
Mirsaidov Mirziyod +3 more
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The light-weight and high-stiffness metal lattice sandwich structure formed by selective laser melting has an important application prospect in aerospace, military and other fields.
ZHANG Bo +5 more
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THREE DIMENSIONAL BUCKLING ANALYSIS OF FG CYLINDRICAL PANELS UNDER VARIOUS THERMAL LOAD CONDITIONS [PDF]
In this paper, buckling analysis of cylindrical panels made of functionally graded material under the action of three types of thermal loads is investigated.
ali ahmadi +2 more
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In this paper an approximate analytical solution to analyze the nonlinear buckling and postbuckling behavior of imperfect functionally graded panels with the Poisson's ratio also varying smoothly along the thickness is investigated.
Dao Van Dung, Le Kha Hoa
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A Ka-Band Cylindrical Paneled Reflectarray Antenna [PDF]
Cylindrical parabolic reflectors have been widely used in those applications requiring high gain antennas. Their design is dictated by the geometric relation of the parabola, which relate the feed location, f, to the radiating aperture, D. In this work, the use of reflectarrays is proposed to increase D without changing the feed location.
greco francesco +3 more
openaire +1 more source
Supersonic Flutter of Circular Cylindrical Shells [PDF]
Various experimental and theoretical studies on the supersonic flutter of circular cylindrical shells are discussed. Results of experiments in the Mach number range 2.5 - 3.5 are presented.
Olson, Mervyn Daniel
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Shielding Performance of Composite Materials Used in Air Vehicles
The metal skin at air vehicles provide an important shielding effectiveness against the effects of high amplitude electromagnetic waves. In recent years, the composite materials with the advantages such as being lighter, causing lower fuel consumption ...
Baha Kanberoğlu, Ahmet Yahya Teşneli
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Influence of geometric imperfections on postbuckling of layered (laminated) composite cylindrical panels has been performed under axial compression load using finite element code, ANSYS and validated experimentally.
Venkata Narayana Yenugula
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This paper presents an analytical approach to investigate the non-linear dynamic response and vibration of an imperfect three-phase laminated nanocomposite cylindrical panel resting on elastic foundations in thermal environments.
Thu Pham Van, Duc Nguyen Dinh
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