Flight Simulation of HS-748 with and without rotodome PArt 2 - Rolls Royce Engine Simulation

摘要

The mathematical models and data used in the offline nonlinear simulation of the HS-748 aircraft with and withoutudrotodome have been described in Part I . In this document, the issues related to the simulation and validation of RollsudRoyce Dart MK 531 Engine against Rolls Royce results are reported . Also the responses of basic and AEW aircraft with single and twin engines operative have been presented . The thrust /engine for different throttle settings speed and altitudes have been . given in table look up form for design and analysis purposes . Simulation studies indicate that there is no deterioration in handling the AEW during asymmetric power or during the failure of port/starboard engine .