21-11. Turbine Engines
In mode TRAINING show all questions of the discipline with correct answers presentation. To go to the next question, click the “Next”.
In mode Exam correct answers are not shown, after choosing the answer, transition to the next question occurs automatically.
1. A “hung start” is the failure of an engine to accelerate to its normal idle speed. It may be caused by:
2. An engine pressure ratio (EPR) can be defined as the ratio of:
3. The propulsive efficiency of a turbojet is the ratio of:
4. The disadvantages of axial flow compressors compared to centrifugal flow compressors are:
1) expensive to manufacture
2) limited airflow
3) greater vulnerability to foreign object damage
4) lower pressure ratio
The combination regrouping all the correct statements is:
5. At constant fuel flow, if engine compressor air is bled off for engine anti-icing or a similar system, the turbine temperature: