An 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.
IN-FLIGHT MEASURED PROPULSION MASS FLOW AND THRUST ON AIRCRAFT
19.01.2023
Patent
Elektronische Ressource
Englisch
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