A method of mission performance analysis for a piston-engined ultralight unmanned helicopter is considered. For each typical flight phase, the approximate analytical expressions for change in helicopter mass are given. The capabilities of the approach being proposed are demonstrated by a numerical example dealing with determining the possible combinations of payload and fuel mass for a given flight plan in the presence of wind.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Mission Performance Analysis for a Piston-Engined Ultralight Unmanned Helicopter


    Weitere Titelangaben:

    Russ. Aeronaut.


    Beteiligte:
    Onushkin, Yu. P. (Autor:in) / Sizov, D. A. (Autor:in) / Ostrovoi, A. V. (Autor:in)

    Erschienen in:

    Russian Aeronautics ; 65 , 1 ; 121-131


    Erscheinungsdatum :

    01.01.2022


    Format / Umfang :

    11 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Britain's first twin-engined helicopter

    Engineering Index Backfile | 1951


    Britain's first twin-engined helicopter

    Engineering Index Backfile | 1951


    Britain's first twin-engined helicopter

    Engineering Index Backfile | 1951


    Britain's first twin-engined helicopter

    Engineering Index Backfile | 1951


    First free-piston-engined tug

    Engineering Index Backfile | 1961