This paper provides fuel consumption analysis of an aircraft during climbing phases with gradual climb procedure. The analysis is based on BADA aircraft performance model and applied to an A320 aircraft climbing performance with varied true airspeeds optimal to the flight altitudes. The acceleration and angle of climb at specific altitudes were consequently varied with altitudes and calculated using numerical techniques. The comparisons of the fuel consumptions of continuous climbing with gradual reduced climb angle procedure and with constant climb angle procedure were presented. The results showed that the gradual climb procedure provides better fuel-saving by 8.1% of the climbing fuel compared to the continuous climb of constant climb angle procedure. It is suggested that the procedure can be improved with optimization of varied true airspeed, acceleration, angle of climb, and aircraft thrust.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Fuel Consumption Analysis of Gradual Climb Procedure with Varied Climb Angle and Airspeed


    Weitere Titelangaben:

    Sustainable aviat.


    Beteiligte:
    Karakoc, T. Hikmet (Herausgeber:in) / Atipan, Siripong (Herausgeber:in) / Dalkiran, Alper (Herausgeber:in) / Ercan, Ali Haydar (Herausgeber:in) / Kongsamutr, Navatasn (Herausgeber:in) / Sripawadkul, Vis (Herausgeber:in) / Atipan, Siripong (Autor:in) / Chomdej, Pawarej (Autor:in)

    Kongress:

    International Symposium On Sustainable Aviation ; 2021 November 25, 2021 - November 27, 2021



    Erscheinungsdatum :

    2023-09-30


    Format / Umfang :

    6 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch







    Easy-climb

    SCOTT RAYMOND E | Europäisches Patentamt | 2018

    Freier Zugriff

    Gaillon hill climb

    Engineering Index Backfile | 1903