Static stability and control characteristics are presented in form of 3-component force data obtained at from 5.8 to 10.1×106; data showing effects of thrust reversal on skin temperatures on fuselage and horizontal tail indicate that these effects were defined by ratio of reversed thrust to momentum of free stream.


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    Title :

    Full-scale wind-tunnel investigation of effects of target-type thrust reverser on low-speed aerodynamic characteristics of single-engine jet airplane


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1959


    Size :

    42 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English