The purpose of the report is to predict drag increment due to rear fuselage upsweep. The results may be applied to the calculation of cruise drag. The research is relevant to military and civil transport aircraft, subcritical Mach numbers.


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    Titel :

    Drag Increment Due to Rear Fuselage Upsweep


    Erscheinungsdatum :

    1980


    Format / Umfang :

    10 pages



    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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