Called the Stagnation Point Reverse Flow Combustor, the Georgia Tech device, originally developed for NASA, significantly reduces NOx and CO emissions in a variety of aircraft engines and gas turbines ...

Called the Stagnation Point Reverse Flow Combustor, the Georgia Tech device is designed for aircraft engines and gas turbines. It burns fuel with NOx emissions below 1 part per million (ppm) and ...

Called the Stagnation Point Reverse Flow Combustor, the Georgia Tech device significantly reduces NOx and CO emissions in a variety of aircraft engines and gas turbines that burn gaseous or liquid ...

Called the Stagnation Point Reverse Flow Combustor, it burns fuel with nitrogen oxide emissions below 1 part per million (ppm) and carbon monoxide emissions lower than 10ppm. The tests were ...