21-11. Turbine Engines
All questions: 172
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Questions for exams: 30
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1. For a fan jet engine, the by-pass ratio is the:
2. A pressure relief valve in an oil system that does not seat correctly would result in:
3. In the axial flow compressor the flow duct is tapered. Its shape is calculated so as to:
4. On landing and prior to shutdown, a gas turbine engine should be run at “ground idle” for a short period. This allows:
5. Each stage of an axial compressor is made up of:
