... due to the transient fuel flow change using the Runge–Kutta method. In this transient performance simulation, the turbine overshoot was predicted. 31 03 2008 09 04 2008 10 02 2009 aerospace computing aerospace engines aerospace propulsion aircraft control control engineering...

...) while showing a good level of adaptivity, readiness, precision, robustness, and stability. 20 09 2006 15 12 2006 gas turbine power stations multi-agent systems control engineering computing power station control power engineering computing MIMO systems blades shafts...

... computing mechanical engineering computing control system synthesis control engineering computing power grids The three-shaft, high-temperature gas-cooled reactor cycle layout used in this study was based on the cycle shown in Fig. 1 . The cycle primarily consists of a precooler (PC), low...