Variable response helicopter is used by Langley Research Center, NASA, to study aircraft handling qualities at low speeds; results of studies of control power and damping are used to construct boundaries or zones showing satisfactory combinations for roll, pitch, and yaw; criteria for minimum acceptable control power and angular velocity damping; criteria which are functions of both gross weight and moments of inertia about respective axis are found to be very useful in VTOL test-bed programs.


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    Titel :

    Helicopters and VTOL aircraft


    Weitere Titelangaben:

    Aero/Space Eng


    Beteiligte:
    Tapscott, R.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1960


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Helicopters and vtol aircraft

    Taylor, John William Ransom | TIBKAT | 1968


    VTOL aircraft and helicopters

    Engineering Index Backfile | 1959


    VTOL aircraft and helicopters

    Engineering Index Backfile | 1961


    Helicopters and VTOL aircraft surveyed

    Engineering Index Backfile | 1960


    Potential of helicopters and VTOL aircraft

    Kelley, B. | Engineering Index Backfile | 1960