Solution investigated by EWR (Entwicklungsring Sued, Munich, West Germany) required engines to be installed in rotatable wing tip pods; basic investigations on VTOL projects with thrust modulation include simulation test with original engines, and simulation with PA CE 231 R computer which investigates complete flight regime from hovering to normal aerodynamic flight and consists of computer and fixed pilot seat with instrumentation similar to that of airplane; results obtained.


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    Titel :

    Contribution to problem of VTOL-control by thrust modulation


    Weitere Titelangaben:

    AIAA -- Tech Papers


    Beteiligte:
    Hafer, X. (Autor:in) / Franke, H. (Autor:in)

    Kongress:

    Simulation for Aerospace Flight Conference ; 1963 VTOL-STOL



    Erscheinungsdatum :

    1963


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :