-
leading to accidents with even loss of precious lives. The combustion chamber and the turbine sections of the gas turbine are most prone to high temperature environmental attack because of having
-
medium/large range aircraft is the ability to pump liquid hydrogen to a suitable pressure for injection into the gas turbine combustion chamber with a pumping system that has mass and volume compatible
-
. The project also explores applicability and testing of the envisaged technologies on cryogenic hydrogen and advanced combustion technologies, aligning with the need for innovative solutions for zero-emission
Searches related to postdoc combustion
Enter an email to receive alerts for postdoc-combustion positions