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6 - Case studies

6.5 - Study of the compression ratio

Figure 6

Figure 6.6 - Study of the compression ratio

In this study, we can consider that the compression ratio is equal to:

ρ = (α′ + α′′ ) / α′′

where ρ is the compression ratio,
α′ is the maximum effective capacity and
α′′ is the dead space.

The unusable volume between the torus and the shutoff valve must be added to the dead space.

The above suggests that the shape of the turbine provides engine breaking.

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