The predicted pitching moment characteristics of the X-29A aircraft are presented for angles of attack from 0 to 20 deg. and Mach numbers of 0.2, 0.6, 0.9, 1.2, and 1.5 for altitudes of sea level, 4572 m (15,000 ft), 9144 m (30,000 ft), and 12,192 m (40,000 ft). These data are for both rigid and flexible aircraft and for the full range of control-surface positions. The characteristics were extracted from a nonlinear, symmetric, flexibilized wind tunnel data base.


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    Title :

    Predicted Pitching Moment Characteristics of X-29A Aircraft


    Contributors:
    G. D. Budd (author)

    Publication date :

    1987


    Size :

    67 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English