The requirements for a new research aircraft to provide in-flight V/STOL simulation were reviewed. The required capabilities were based on known limitations of ground based simulation and past/current experience with V/STOL inflight simulation. Results indicate that V/STOL inflight simulation capability is needed to aid in the design and development of high performance V/STOL aircraft. Although a new research V/STOL aircraft is preferred, an interim solution can be provided by use of the X-22A, the CH-47B, or the 4AV-8B aircraft modified for control/display flight research.


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    Titel :

    V/STOL flight simulation


    Erscheinungsdatum :

    1979-11-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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