Numerical Simulation of 3D Unsteady Flowfield in Aft-Finocyl Solid Rocket Motor
The flowfield inside the second solid stage of the European launch vehicle VEGA is
simulated with a full 3D unsteady flow solver in order to characterize the unsteadinesses,
aero-acoustics and dynamics loads resulting from the growth of complex vorticity patterns
in the internal flow of the aft-finocyl solid rocket motor.






