An F100 augmented turbofan engine equipped with digital electronic engine control (DEEC) system was evaluated. The engine was equipped with a specially modified augmentor to provide improved steady state and transient augmentor capability. The combination of the DEEC and the modified augmentor was evaluated in sea level and altitude facility tests and then in four different flight phases in an F-15 aircraft. The augmentor configuration, logic, and test results are presented.
Augmentor transient capability of an F100 engine equipped with a digital electronic engine control
01.03.1984
Aufsatz (Konferenz)
Keine Angabe
Englisch
SAE Technical Papers | 1980
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