Common use of Stress analysis Clause in Contracts

Stress analysis. The stresses in the tangential and longitudinal direction of the cylinder in the composite and in the liner shall be calculated. The pressures used for these calculations shall be zero, working pressure, test pressure and design burst pressure. The calculations shall use suitable analysis techniques to establish stress distribution throughout the cylinder.

Stress analysis. The stresses in the tangential and longitudinal direction of the cylinder in the composite and in the liner after pressure shall be calculated. The pressures pressure used for these calculations shall be zero, working pressure, 10 per cent of working pressure, test pressure and design burst pressure. The limits within which autofrettaging pressure must fall shall be calculated, The calculations shall use suitable analysis techniques using thin-shell theory taking account of non-linear material behaviour of the liner to establish stress distribution throughout distributions at the cylinderneck, transition regions and the cylindrical part of the liner.

Stress analysis. The stresses in the tangential and longitudinal direction of the cylinder in the composite and in the liner after pressure shall be calculated. The pressures pressure used for these calculations shall be zero, working pressure, 10 per cent of working pressure, test pressure and design burst pressure. The limits, within which auto-frettaging pressure shall fall, shall be calculated. The calculations shall use suitable analysis techniques using thin-shell theory taking account of non-linear material behaviour of the liner to establish stress distribution throughout distributions at the cylinderneck, transition regions and the cylindrical part of the liner.

Stress analysis. The stresses in the tangential and longitudinal direction of the cylinder in the composite and in the liner after pressure shall be calculated. The pressures pressure used for these calculations shall be zero, working pressure, 10 per cent of working pressure, test pressure and design burst pressure. The limits within which auto-frettaging pressure shall fall shall be calculated. The calculations shall use suitable analysis techniques using thin-shell theory taking account of non-linear material behaviour of the liner to establish stress distribution throughout distributions at the cylinderneck, transition regions and the cylindrical part of the liner.

Stress analysis. The stresses in the tangential and longitudinal direction of the cylinder in the composite and in the liner after pressure shall be calculated. The pressures pressure used for these calculations shall be zero, working pressure, 10 per cent of working pressure, test pressure and design burst pressure. The limits, within which auto- frettaging pressure shall fall, shall be calculated. The calculations shall use suitable analysis techniques using thin-shell theory taking account of non- linear material behaviour of the liner to establish stress distribution throughout distributions at the cylinderneck, transition regions and the cylindrical part of the liner.

Stress analysis. The stresses in the tangential and longitudinal direction of the cylinder in the composite and in the liner after pressure shall be calculated. The pressures pressure used for these calculations shall be zero, working pressure, 10 per cent of working pressure, test pressure and design burst pressure. The limits within which autofrettaging pressure must fall shall be calculated, The calculations shall use suitable analysis techniques using thin-shell theory taking account of non-linear material behaviourbehavior of the liner to establish stress distribution throughout distributions at the cylinderneck, transition regions and the cylindrical part of the liner.

Stress analysis. The stresses in the tangential and longitudinal direction of the cylinder in the composite and in the liner after pressure shall be calculated. The pressures pressure used for these calculations shall be zero, working pressure, 10 percent of working pressure, test pressure and design burst pressure. The limits within which autofrettaging pressure must fall shall be calculated, The calculations shall use suitable analysis techniques using thin-shell theory taking account of non-linear material behavior of the liner to establish stress distribution throughout distributions at the cylinderneck, transition regions and the cylindrical part of the liner.

Stress analysis. The stresses in the tangential and longitudinal direction of the cylinder in the composite and in the liner after pressure shall be calculated. The pressures pressure used for these calculations shall be zero, working pressure, 10 per cent of working pressure, test pressure and design burst pressure. The limits within which autofrettaging pressure must fall shall be calculated, The calculations shall use suitable analysis techniques using thin-shell theory taking account of non-linear material behavior of the liner to establish stress distribution throughout distributions at the cylinderneck, transition regions and the cylindrical part of the liner.