During the first reporting period research concentrated on finishing the modeling work required for a representative model of a scramjet propulsion system for hypersonic vehicles. An existing hypersonic propulsion code was adjusted to the winged-cone configuration. In this process the complete force and moment calculation was revised. The advantageous feature of the code to account for angle of attack variations was then used to compute the thrust, lift, and pitching moment contributions of the propulsion system not only for various Mach numbers and fuel equivalence ratios, but also for different angles of attack.


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    Title :

    Research in Robust Control for Hypersonic Vehicles


    Contributors:
    A. J. Calise (author) / H. Buschek (author)

    Publication date :

    1992


    Size :

    45 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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