Ground-based flight simulation has been used successfully to support low altitude, asymmetric thrust, high angle of attack flight testing of the Grumman/Navy F-14A. The high risk nature of this flight testing, while representing a prime example of the application of simulation in the flight test environment, nonetheless generated particular problems regarding simulation fidelity and utilization requirements. As a result, new simulation capabilities were developed specifically for flight test support applications and were fully integrated into existing flight test computing/data analysis facilities. Results from the F-14 high angle of attack flight testing are used to illustrate how simulation can significantly enhance overall flight test safety and productivity. Using simulation support, an efficient test program was completed on time and allowed the F-14's departure characteristics to be safely demonstrated at angles of attack greater than 60 degrees with full engine thrust asymmetry at altitudes below 10,000 ft (3030 m).


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    Titel :

    Utilization of Simulation to Support F-14A Low Altitude High Angle of Attack Flight Testing


    Beteiligte:
    P. Conigliaro (Autor:in) / R. Goodman (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    15 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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