The invention relates to an aerodynamic engine assembly, which belongs to the technical field of aerodynamics and comprises an engine shell, a bottom shell, a cylinder body, a cylinder cover, a crankshaft, a flywheel, a clutch and a speed changing box. A valve component is disposed on the cylinder cover, the cylinder cover is provided with an air inlet channel and an air exhaust channel, the air inlet channel and the air exhaust channel are connected with an air inlet header pipe and an air exhaust header pipe, a high-pressure air inlet channel is further disposed on the cylinder cover, a one-way valve is disposed in the high-pressure air inlet channel, and the high-pressure air inlet channel is connected with a high-pressure controller via a high-pressure air source controlling device. The aerodynamic engine assembly is characterized in that a turbocharger is mounted between the air inlet header pipe and the air exhaust header pipe, an air inlet end of the turbocharger is connected with the atmosphere, the turbocharger is connected with a power generator, the power generator is connected with a storage battery, and a turbine generator set which is in step layout is mounted on a tail gas exhaust tube of the turbocharger and is connected with the storage battery. In conclusion, the aerodynamic engine assembly has the advantages of simple structure, reasonable design, capabilities of controlling high-pressure air sources to supply air uniformly, supplementing air pressure loss and saving energy, and the like.