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For the 7075 aluminum alloy plate, the longitudinal modulus of elasticity E [Pa] (Young\'s modulus) has the value of 75 GPa, and ν, the Poisson\'s ratio is 0.33. Using the density calculation formula [10], a density of 2810 kg/m3 was obtained for the 7075-aluminum
− To give background to calculation methods for aluminium members in order to understand the specific behaviour of statically loaded aluminium alloy structures.
optimizing stretch rate on the basis of residual stress distribution law. By comparing the variation principle of residual stress in length direction, the size range of three
1 nov 2012 A mathematical model is developed to calculate the residual stress in stretched aluminum alloy thick plate. It is based on balance of stresses, two
1 ago 2014 A mathematical model is developed to calculate the residual stress in stretched aluminum alloy thick plate. It is based on balance of stresses, two
29 mar 2012 Numerical simulation combined with experimental test was carried out to analyze the pre-stretching process of the 7075 aluminum alloy sheet, from which the
Deflection Calculator for Aluminium Profiles. Convenient tool for calculating the deflection of aluminium profiles as a function of load. The three most common load scenarios are
The plate stretching system allows the efficient production of high-quality, evenly stretched sheets of aluminum alloys in strip thickness range of 0.8 to 8.0 mm and a length of
method to predict the FLC of aluminum alloy sheet was verified. Finally, the predicted FLC was applied to analyze the fracture of the curved part in the stretch-forming process,
In the simulation, actual conditions are taken into account, aluminum plates are not directly pulled at the two ends but stretched with two groups of clamps, and the stretching
For 7075 aluminum alloy plate, longitudinal modulus of elasticity E [Pa] (Young\'s modulus) has value of 75 GPa, and ν, Poisson\'s ratio is 0.33. Using density calculation formula [10], a density of 2810 kg/m3 was obtained for 7075-aluminum alloy plate tested. For yield stress level,
− To give background to calculation methods for aluminium members in order to understand the specific behaviour of statically loaded aluminium alloy structures. Prerequisites: − Basic structural mechanics and design philosophy − Structural aluminium alloys and product forms
optimizing stretch rate on the basis of residual stress distribution law. By comparing the variation principle of residual stress in length direction, the size range of three deformation areas and elimination percentage of residual stress were
29 mar 2012 Numerical simulation combined with experimental test was carried out to analyze the pre-stretching process of the 7075 aluminum alloy sheet, from which the stress variation curves and residual stress of aluminum alloy sheet in
1 ago 2014 A mathematical model is developed to calculate the residual stress in stretched aluminum alloy thick plate. It is based on balance of stresses, two-dimensional plasticity and a conception
1 nov 2012 A mathematical model is developed to calculate the residual stress in stretched aluminum alloy thick It is based on balance of stresses, two-dimensional plasticity and a conception of free size. The model is verified against the published experiments performed on 7075 aluminum
The plate stretching system allows the efficient production of high-quality, evenly stretched sheets of aluminum alloys in strip thickness range of 0.8 to 8.0 mm and a length of 4,000-6,400
method to predict the FLC of aluminum alloy sheet was verified. Finally, the predicted FLC was applied to analyze the fracture of the curved part in the stretch-forming process, which provided the theoretical basis for judging the fracture defects generated in the stretch-forming process. 2. Uniaxial Tensile
In the simulation, actual conditions are taken into account, aluminum plates are not directly pulled at the two ends but stretched with two groups of clamps, and the stretching clamps are defined as rigid body. The stretching process is divided into three stages: clamping, stretching and releasing, as shown in Fig.
Engineering Analysis Menu Flat Plates Stress, Deflection Equations and Calculators: The follow pages contain engineering design calculators that will determine the amount of deflection and stress a flat plate of known thickness will deflect under the specified load and
optimizing stretch rate on the basis of residual stress distribution law. By comparing the variation principle of residual stress in length direction, the size range of three deformation areas and elimination percentage of residual stress were
Engineering Analysis Menu Flat Plates Stress, Deflection Equations and Calculators: The follow pages contain engineering design calculators that will determine the amount of deflection and stress a flat plate of known thickness will deflect under the specified load and
1 nov 2012 A mathematical model is developed to calculate the residual stress in stretched aluminum alloy thick It is based on balance of stresses, two-dimensional plasticity and a conception of free size. The model is verified against the published experiments performed on 7075 aluminum
For 7075 aluminum alloy plate, longitudinal modulus of elasticity E [Pa] (Young\'s modulus) has value of 75 GPa, and ν, Poisson\'s ratio is 0.33. Using density calculation formula [10], a density of 2810 kg/m3 was obtained for 7075-aluminum alloy plate tested. For yield stress level,
The plate stretching system allows the efficient production of high-quality, evenly stretched sheets of aluminum alloys in strip thickness range of 0.8 to 8.0 mm and a length of 4,000-6,400
In the simulation, actual conditions are taken into account, aluminum plates are not directly pulled at the two ends but stretched with two groups of clamps, and the stretching clamps are defined as rigid body. The stretching process is divided into three stages: clamping, stretching and releasing, as shown in Fig.
− To give background to calculation methods for aluminium members in order to understand the specific behaviour of statically loaded aluminium alloy structures. Prerequisites: − Basic structural mechanics and design philosophy − Structural aluminium alloys and product forms
29 mar 2012 Numerical simulation combined with experimental test was carried out to analyze the pre-stretching process of the 7075 aluminum alloy sheet, from which the stress variation curves and residual stress of aluminum alloy sheet in
1 ago 2014 A mathematical model is developed to calculate the residual stress in stretched aluminum alloy thick plate. It is based on balance of stresses, two-dimensional plasticity and a conception
method to predict the FLC of aluminum alloy sheet was verified. Finally, the predicted FLC was applied to analyze the fracture of the curved part in the stretch-forming process, which provided the theoretical basis for judging the fracture defects generated in the stretch-forming process. 2. Uniaxial Tensile
