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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Drag Increment Due to Rear Fuselage Upsweep


    Publication date :

    1980


    Size :

    10 pages



    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Effect of upsweep angle on the mean flowfield of a simulated cargo fuselage

    Aultman, Matthew T. / Ranjan, Rajesh / Gaitonde, Datta V. | AIAA | 2020


    Aircraft fuselage configuration with upwardly deflected rear fuselage

    REWERTS STEPHEN D / BELL JEFFERY C / LUNDSTROM MICHAEL E | European Patent Office | 2023

    Free access

    Tailscrape on rear fuselage

    Emerald Group Publishing | 2000


    Rear fuselage of airplane

    LI YAOHUA / SHU ZHAOXIN / OUYANG DI | European Patent Office | 2022

    Free access