A comparison between Full Potential and Euler numerical solutions for
2D transonic unsteady flow is presented. The pros and cons of the pote
ntial model are discussed and the main features of both computational
methods are summarised. The comparison is done for a Naca 0012 aerofoi
l oscillating in pitch at a freestream Mach number ranging from 0.755
to 0.825, in order to investigate the limit of application of the pote
ntial approximation in an unsteady flow.