Flight Simulation of HS - 748 with and without rotodome Part 3- Aerostatic Model Formulation

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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