The figure below illustrates a typical single spool axial flow turbojet engine.
ID: 2323226 • Letter: T
Question
The figure below illustrates a typical single spool axial flow turbojet engine. It is required to calculate the distribution of the thrust force for each component (compressor, diffuser, combustion chamber, turbine, jet pipe, and nozzle) during ground run. Prove that the sum of these thrust forces is equal to the thrust force developed by the engine using the usual thrust force equation.
Figure 1 Thrust distribution for a typical single spool turbojet engine
Explain how you have applied Newton’s 3rd law.
Explanation / Answer
The figure below illustrates a typical single spool axial flow turbojet engine. It is required to calculate the distribution of the thrust force for each component (compressor, diffuser, combustion chamber, turbine, jet pipe, and nozzle) during ground run. Prove that the sum of these thrust forces is equal to the thrust force developed by the engine using the usual thrust force equation.
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