Matrics (multi-component aircraft transonic inviscid computation system): preliminary document

In the present document the pre-design will be presented of the system MATRICS (Multi-component Aircraft Transonic Inviscid Computation System). The system will be able to calculate the inviscid steady transonic flow about complex transport aircraft under cruise conditions; both jet-aircraft and propeller-aircraft can be simulated. As such the system will contribute to the efficient design of aerodynamically competitive aircraft.