Our long term objective is the development of a fast and sound methodology for simulating the dynamic aeroelastic response of an aircraft during three-dimensional high-G maneuvers in transonic and supersonic airstreams. Our focus is on AIR FORCE relevant problems exemplified by a transonic/supersonic lifting body geometry performing complex multi-G maneuvers at a free-stream Mach number M00 ranging between 0.7 and 3 (0.7 </- M(infinity) </- 3).


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    Title :

    Numerical Simulation of Three-Dimensional High-G Dynamic Maneuvers of a Complete and Flexible Aircraft Configuration


    Contributors:
    C. Farhat (author)

    Publication date :

    1999


    Size :

    10 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English