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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