Sökning: "afterbody drag"

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  1. 1. OPTIMIZATION OF NOZZLE SETTINGS FOR A FIGHTER AIRCRAFT

    Master-uppsats, Mälardalens högskola/Industriell ekonomi och organisation

    Författare :Alexander Stenebrant; Nor Al-Mosawi; [2019]
    Nyckelord :Low-bypass turbofan; afterburner; convergent-divergent nozzle; afterbody drag; computational fluid dynamics.;

    Sammanfattning : Most fighters use the convergent-divergent nozzle configuration to accelerate into the supersonic realm. This nozzle configuration greatly increases the thrust potential of the aircraft compared to the simpler convergent nozzle. LÄS MER