A third axial compressor stage added for increased pressure ratio.

The X and subsequent engines had a second axial compressor stage added.

Air passes through an inlet and is then compressed by an axial compressor.

This is process is very similar to how an axial compressor works, only in reverse.

Key to the engine's working cycle was an axial compressor of then-unique construction.

An axial compressor is a pressure producing machine.

Axial compressors can have high efficiencies; around 90% polytropic at their design conditions.

Some turboprop engines use an impeller instead of an axial compressor.

The reason for using an impeller instead of an axial compressor is that the engine's length can be reduced.

A simplified civilian version of the J79 featuring an axial compressor, it was developed in two versions.

As of the Astazou X, the engine received a second axial compressor stage.

He was also an author of the widely cited paper "Boundary layer development in axial compressors and turbines."

Accessories were grouped around the axial compressor which conveniently narrowed towards the rear.

It was a single-shaft turbojet with a seven-stage axial compressor.

Axial compressors consist of rotating and stationary components.

Representation of the performance characteristics of axial compressor can be done by following parameters:

In the gas-generator section air enters through a inlet screen into the low-pressure axial compressor.

Axial compressors, known as superchargers, have also been used to boost the power of automotive reciprocating engines.

For all of these reasons, axial compressors on modern jet engines are considerably more complex than those on earlier designs.

The RAE continued working on axial compressor design after the F.2 success.

Axial compressors rely on spinning blades that have aerofoil sections, similar to aeroplane wings.

To achieve different pressure ratios, axial compressors are designed with different numbers of stages and rotational speeds.

The Dovern was the next design, featuring a nine-stage axial compressor and single-stage turbine.

Include additional axial compressor stage.

In a practical gas turbine, gases are first accelerated in either a centrifugal or axial compressor.