For a given shape of an Aluminium diaphragm and its thcikness, at precisely what tensile stress will it rupture in case of sudden development of pressure differenitial across its thickness. Can it be related to the static UTS of Al foil. If yes then how...
If an impact testing equipment is required for this then how to translate its result into MPa (Static Tensile stress). The reason is that usually only static UTS is available in tables