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Showing 1 to 1 of 1 for “"specific power takeoff"”.
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A Design Study of Single-Rotor Turbomachinery Cycles
… thrust for aircraft engines and supply shaft power for various applications. They consist of three main components. That is, a compressor followed by a combustion chamber (burner) and a turbine. Both turbine and compressor components are either axial or centrifugal (radial) in design. The …