thruthefence,
The aluminum alloys used for cast cylinder heads is normally a heat-treatable alloy. It develops its mechanical properties through a solution heat-treatment, quench and age hardening process. The heating and cooling cycles the head undergoes during normal operation is very similar to the artificial age hardening heat-treatment process that gives it its initial strength. So, in effect, it gets a heat treatment every time it is thermally cycled.
Aluminum alloys exposed to high temperatures and sustained loads can experience a phenomenon referred to as "creep". But this is not something a cylinder head would normally experience.
The excessive strains that the joint between an aluminum cylinder head with ferrous fasteners might experience is mostly due to the CTE mismatch between the fasteners and the clamped aluminum head material. The relative stiffness of the two mating parts is a function of the two mating materials MoE and their section properties, and has absolutely nothing to do with tensile strength as the article suggests. However, the compressive spring rate of the head material is normally much greater than the tension spring rate of the fastener, so the fastener is more likely to fail (plastically yield) first. The tensile strength of the cylinder head bolts on most (cost sensitive) production engines is marginal under the best of conditions, so it is quite easy to plastically yield them. And the head bolt is threaded into the block, not the head. Even if the block is aluminum, the head bolt thread engagement produces a thread root shear strength far in excess of the tensile strength of the bolt body.
Any plastic yield of the fastener relieves the preload on the head gasket joint, the gasket loses its seal, and the leaking, high-temp exhaust gases cause a local overheating of the surrounding structures. That's the typical failure mode.
Even if an aluminum cylinder head somehow experiences localized annealing, it is no small task to re-heat-treat it as the article would suggest. To do so would require a full solution heat treat, quench, and age hardening cycle. This would mean removing the ferrous valve seats and bronze (or iron) valve guides. The heat treat cycle would also likely stress relieve the head structure initially, and then produce further distortions when it is quenched. Thus it would likely require re-machining of all close tolerance surfaces, such as cam journals, deck surface, valve guide bores and valve seat c'bores.
The article you linked had some accurate information, but it also had some very misleading information. That's just my opinion.
Good luck,
Terry