International Journal of Aerospace Engineering / 2019 / Article / Fig 3

Research Article

The Nonlinear Single Controller of DGEN380 Aero Engine Design

Figure 3

The results of the identification of mapping relation between the rotary. (a) The corresponding relation between the consumed work by fan and low rotor speed (spot-component test data, line-identification curve). (b) The corresponding relation between the produced work by LPT and low rotor speed (spot-component test data, line-identification curve). (c) The corresponding relation between the consumed work by HPC and high rotor speed (spot-component test data, line-identification curve). (d) The corresponding relation between the produced work by HPT and high rotor speed (spot-component test data, line-identification curve).
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