;Contents: Flying qualities requirements; Selection of baseline flight condition; Selection of coefficient variation ranges; Technical approach; Coefficient prediction accuracy requirements; Lateral-directional parameter variation data; Longitudinal parameter variation data; Coefficient accuracy requirements -- unaugmented aircraft; Coefficient accuracy requirements -- baseline augmented aircraft.


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    Title :

    STOL Tactical Aircraft Investigation, Externally Blown Flap. Volume V. Part 3. Stability and Control Derivative Accuracy Requirements and Effects of Augmentation System Design


    Contributors:

    Publication date :

    1973


    Size :

    200 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English