The TFAST project covered very wide range of knowledge starting from the basic research to more applied flow configurations. New knowledge generated in this project casts new light on the possibilities of flow control methods in reducing negative effects of shock wave interaction with laminar boundary layer. On the other hand application of flow control devices in the laminar boundary layer, just to inspire transition, is a valuable result. As usually in such complex flow structure the results are strongly case dependent, but the complexity of the presented approach shows great potential for improvements and provides a good basis for future research
