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

Madhuranath, Padma and Sridhar, JK and Satyabhagavan, B (1989) Flight Simulation of HS-748 with and without rotodome PArt 2 - Rolls Royce Engine Simulation. Project Report. NAL, Bangalore.

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    Abstract

    The mathematical models and data used in the offline nonlinear simulation of the HS-748 aircraft with and without rotodome have been described in Part I . In this document, the issues related to the simulation and validation of Rolls Royce 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 .

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Flight Simulation;Mathematical Models;Aircraft Data Engine Simulation;Engine Failure
    Subjects: AERONAUTICS > Aircraft Design, Testing & Performance
    Division/Department: Systems Engineering Division, Systems Engineering Division, Systems Engineering Division
    Depositing User: Mr Nisanth
    Date Deposited: 16 Jul 2012 11:52
    Last Modified: 16 Jul 2012 11:52
    URI: http://nal-ir.nal.res.in/id/eprint/10578

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