High auxiliary air flow requirements of high speed aircraft place increased emphasis on design of efficient outlets through which air is returned to outside stream; use of small outlets to establish desired pressure fields in certain areas also finds application in boundary layer and aircraft control systems.


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    Title :

    Preliminary investigation of aerodynamic characteristics of small inclined air outlets at transonic mach numbers


    Additional title:

    NACA -- Tech Note


    Contributors:
    Dewey, P.E. (author)


    Publication date :

    1955


    Size :

    21 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :