The report promotes an understanding of V/STOL analysis for simulation purposes and develops equations of motion compatible to either analogue or real time digital solution. A general set of equations of motion are developed in which axis systems and aerodynamic coefficients are minimized. Equations of motion are then developed for five different V/STOL aircraft wherein the need for additional axis systems and aerodynamic coefficients for a particular V/STOL configuration is developed. (Author)


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    Title :

    Simulation of Helicopter and V/STOL Aircraft. Volume II. V/STOL Analysis Report. Study, Equations of Motion of Vertical/Short Take-off and Landing Operational Flight/Weapon System Trainers


    Contributors:
    W. McIntyre (author)

    Publication date :

    1963


    Size :

    2 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English