A time domain method has been developed for treatments of vortex dynam
ics in all classes of blade-blade interaction problems. A new vortex i
mpingement condition is introduced to the discrete vortex tracking sch
eme and was found most effective in handling the vortex-airfoil intera
ction and the blade-blade interaction (BBI) problems. Present results
are verified with all classical solutions and are found in good agreem
ent with almost all existing solutions. The present BBI study conclude
s that any front blade movement mill induce a strong interaction betwe
en the make and the rear blade; hence, it alters drastically the lift
response and the wake structure. Any rear blade movement only induces
a weak interaction, hence rendering the blade system ineffective.