I would have to disagree with you Perennial, maybe it's mostly semantics, but either way. I would argue that no grid type has better "accuracy" than another type. Tets can give better answers than hex meshes, and vice versa. I will agree that using structured hex meshes give you ability to use high order of accuracy; but that concept is not directly related to the actual accuracy. Using first-order tet elements with localized bunching can give you a better answer in less computation time than hexes. Again though, it's on a case by case basis.
However, in the field of aeroacoustics, I would say that structured hexes are a necessity, when possible. This goes back to the concept of order of accuracy. Order of accuracy is defined as the rate at which the error decreases with decreasing mesh spacing. The error can decrease exponentially though for higher order schemes. For example, when halfing the grid spacing, for a single order scheme, the error decreasing by:
[tex]\epsilon = (2)^1 = 2[/tex]
Where 2 is the grid density factor, and 1 is the order of the scheme being used. If I were to use a 6th order DRP scheme, I would expect the error to drop by:
[tex]\epsilon = (2)^6 = 64[/tex]
Now that's not to say that a higher order scheme will always out perform a low order scheme, because that's not the case. In fact, at large grid spacing, one can show that a low order scheme actually provides a better solution with less error. However, if one needs very very high accuracy (as in the case of aeroacoustics), then one can easily see that in order to get the desired accuracy from a first-order scheme, the grid density will need to become ridiculous; whereas there will be a crossing point where the high-order scheme becomes less computationally heavy.
IMHO, CFD is still very much a black or grey art/practice, where the user really needs to understand much of what's going on behind the scenes in order to determine how much to believe the answer.