The use of a computer program for a comprehensive analytical model of rotorcraft aerodynamics and dynamics is described. The program calculates the loads and motion of helicopter rotors and airframe. First the trim solution is obtained, then the flutter, flight dynamics, and/or transient behavior can be calculated. Either a new job can be initiated or further calculations can be performed for an old job.


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    Title :

    A Comprehensive Analytical Model of Rotorcraft Aerodynamics and Dynamics. Part 2: User's Manual


    Contributors:
    W. Johnson (author)

    Publication date :

    1980


    Size :

    97 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English