Aircraft minimum flying speed, as determined by actual flight test, is published in aircraft handbooks for pilot guidance. The test flight results are used to determine and confirm take-off and landing speeds, field lengths, left-hand portion of the maneuvering envelopes (V-n diagram), etc. Determination of the absolute minimum flying speed of an aircraft on the other hand, has not been of prime importance in flight test. In the present analysis digital simulation allowed by systematic study of not only the minimum flying speed as defined by Federal Aviation Regulations but also the absolute minimum flying speed attainable in steady, unaccelerated flight. The study included such effects as deceleration rate, rate of change of elevator angle, aircraft weight and pitch moment of inertia. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Evaluation of Minimum Aircraft Flying Speed by Digital Simulation


    Beteiligte:
    C. W. Saul (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    73 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Minimum speed and safe flying

    Gymnich, A. | Engineering Index Backfile | 1928


    Minimum speed and safe flying

    Gymnich, A. | Engineering Index Backfile | 1928


    High speed aircraft flying limitations and handling problems

    Morgan, F.W. | Engineering Index Backfile | 1947


    HIGH-SPEED FLYING METHOD AND RING WING AIRCRAFT

    LUO CONGGUI / ZHENG XIAOYAN | Europäisches Patentamt | 2021

    Freier Zugriff