A method (600) of thrust control for an airbreathing jet engine (50). The method comprises obtaining a demanded thrust setting, obtaining a value of static pressure at a first axial location (35) of a combustion chamber (30) of the airbreathing jet engine ...

A compression ignition internal combustion engine includes: a cylinder block and a cylinder head; a piston including a cavity that defines a combustion chamber in cooperation with the cylinder block and the cylinder head; and a nozzle for injecting fuel in...