In-flight measured propulsion mass flow and thrust on aircraft

Lowe, K. ToddByun, Gwi BoKrejmas, Albert2024-12-122024-12-122024-10-22https://hdl.handle.net/10919/123786An aircraft includes a gas turbine engine and an optically-based measurement system. The gas turbine engine is configured to ingest a first mass flow and to exhaust a second mass flow. The optically-based measurement system is configured to determine the first and second mass flows in response to performing an imaging process on the gas turbine engine.application/pdfenIn CopyrightIn-flight measured propulsion mass flow and thrust on aircraftPatentLowe, Kevin [0000-0002-0147-4641]12123313B2