1. A turbojet engine used to drive an external propeller.

2. The stability, reliability and performance of two spool turbojet engine will be affected by the matching correlation between 1st and 2nd turbine nozzle areas and engine nozzle area.

3. Many off-design condition phenomena of a turbojet engine are related with the variation of incidence angles at front and rear compressor stages.

4. A model for 100N class micro turbojet engine is established. Software and hardware system design of the controller is accomplished by using robust control algorithm.

5. Stimulation to the pilotless aircraft turbojet engine proves several advantages of this controlling method, such as good robustness, sensitive response, and minimal stable error.

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6. A brief view and results of tests for the effects of the inlet total pressure distortion on the performance and the stability of a two-spool turbojet engine are presented.

7. A stage by stage mathematical model of the compressor in a turbojet engine is developed based on the control volume theory.

8. The rocket sled test was carried out for overall investigating the dynamic process of missile turbojet engine starting and accelerating.

9. Experiments were performed to investigate surge problem of a single shaft axial flow turbojet engine during throttling.

10. This paper covers the designs of Hardware in the Loop Simulation (HILS) testing of minitype turbojet engine digital control regulator, and hardware and software configurations.

11. As an example, a robust control law is designed to the twin-spool turbojet engine system using the given method. The result shows that the given method is feasible.

12. This paper presents the test plan, the results of the station parameters measurement for a typical turbojet engine and the analysis of measurement results.

13. The improved and modification designs were conducted for a turbojet engine.

14. The rocket sled test can imitate the dynamic conditions of missile launching, it is very important for missile turbojet engine design.

15. Simulations on the nonlinear model of the twin spool turbojet engine aerothermodynamics are conducted to verify the disturbance rejection and tracking performance.

16. The process of loosing compressor aerodynamic stability in a turbojet engine was analyzed using the correlation integral method.

17. The design and test results of the new type high-subsonic speed submerged and semi-submerged intakes for cruise missile propelled by a turbojet engine have been introduced.

18. Among these superalloys, nickel-base superalloys are widely used as thermal components in the turbojet engine.

19. It was powered by an Allison J 33 A turbojet engine.

20. A special instument is presented for monitoring the transient process in a turbojet engine, which is called "transient operating line indicator".