Simulation data are reported for the purpose of programming the flight simulator for advanced aircraft for tests of the lift/cruise fan V/STOL Research Technology Aircraft. These simulation tests are to provide insight into problem areas which are encountered in operational use of the aircraft. A mathematical model is defined in sufficient detail to represent all the necessary pertinent aircraft and system characteristics. The model includes the capability to simulate two basic versions of an aircraft propulsion system: (1) the gas coupled configuration which uses insulated air ducts to transmit power between gas generators and fans in the form of high energy engine exhaust and (2) the mechanically coupled power system which uses shafts, clutches, and gearboxes for power transmittal. Both configurations are modeled such that the simulation can include vertical as well as rolling takeoff and landing, hover, powered lift flight, aerodynamic flight, and the transition between powered lift and aerodynamic flight.


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    Title :

    Mathematical Model for Lift/Cruise Fan V/STOL Aircraft Simulator Programming Data


    Contributors:
    M. P. Bland (author) / B. Fajfar (author) / R. K. Konsewicz (author)

    Publication date :

    1976


    Size :

    263 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Mathematical model for lift/cruise fan V/STOL aircraft simulator programming data

    Bland, M. P. / Fajfar, B. / Konsewicz, R. K. | NTRS | 1976


    Fan Lift-Cruise V/STOL Aircraft

    J. M. Peterson | NTIS | 1976


    Propulsion System Mathematical Model for a Lift/Cruise Fan V/STOL Aircraft

    G. L. Cole / J. F. Sellers / B. E. Tinling | NTIS | 1980


    Propulsion system mathematical model for a lift/cruise fan V/STOL aircraft

    Cole, G. L. / Sellers, J. F. / Tinling, B. E. | NTRS | 1980