Madhuranath, Padma and Sridhar, JK and Srinath Sastry, CV (1989) Flight Simulation of HS - 748 with and without rotodome Part 3- Aerostatic Model Formulation. Project Report. NAL, Bangalore.
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Abstract
The mathematical models and data used in the off-line flight simulation of the rotodomed aircraft have been described in detail in Part 1 . The issues related to the Rolls Royce Engine simulation studies have been presented in Part 2 . In this document, static wind tunnel test data generated at H .A .L and considered as acceptable by BAE has been used as a reference data for verifying and formulating the aero-static model and associated data for HS-748 and AEW configurations . The resulting static model has been combined with dynamic model to arrive at an overall representative Aero model for use in flight simulation studies . This procedure is vital for unusual aircraft configurations as most of the data at design stage is available only from static wind tunnel tests.
| Item Type: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | Flight Simulation;Mathematical Models Aircraft Data;Wind tunnel Data |
| Subjects: | AERONAUTICS > Aerodynamics AERONAUTICS > Aircraft Design, Testing & Performance |
| Division/Department: | Systems Engineering Division, Systems Engineering Division, Systems Engineering Division |
| Depositing User: | Mr Nisanth |
| Date Deposited: | 17 Jul 2012 10:40 |
| Last Modified: | 17 Jul 2012 10:40 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10581 |
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