Static pressure coefficient distributions on the forebody, afterbody, and nozzles of a 1/12 scale F-15 propulsion model were determined. The effects of nozzle power setting and horizontal tail deflection angle on the pressure coefficient distributions were investigated.


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    Title :

    Fuselage and Nozzle Pressure Distributions on a 1/12-Scale F-15 Propulsion Model at Transonic Speeds


    Contributors:

    Publication date :

    1979


    Size :

    140 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English