The aerothermodynamic control of aircraft jet engines was investigated in order to study automatic (without taking the engine apart) indication and localization of propulsion system failures. The problem of the theoretical values for propulsion control is discussed and an analysis of the influencing factors was made. Failure localization is discussed and the measurement method and data collection and data processing techniques are considered. Finally, experimental investigations are presented.
Theoretical and Experimental Investigations of Aerothermodynamic Control of Aircraft Jet Propulsion Systems Theoretische und Experimentelle Untersuchungen Zur AERO-Thermodynamischen Ueberwachung von Luftfahrt-Strahltriebwerken
1974
159 pages
Report
Keine Angabe
Englisch