The Aircraft Euler Method, so-called AIRPLANE code, is a finite elemen
t based technique for solving the Euler equations combined with a meth
od for constructing tetrahedral meshes. The attractivity of this appro
ach along with the demand of shortened turnaround times motivate a mas
sively parallel implementation. The numerical method is described and
the guidelines for the parallelization strategy are outlined. The mass
ively parallel realization is carried out with PARMACS as a message pa
ssing programming environment. Performance results are presented on di
fferent massive parallel platforms considering a data set of computati
onal meshes of different size. However, these results have to be regar
ded as preliminary since no access to the modern massively parallel co
mputers could be arranged so far.