Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Three-dimensional boundary-layer flow over a flat delta wing at a moderate angle of attack.


    Author / Creator :

    LI, T. Y. /OHIO STATE U., DEPT. OF AERONAUTICAL AND ASTRONAUTICAL ENGINEERING, COLUMBUS, OHIO/., POLAK, A. /CINCINNATI, U., DEPT. OF AEROSPACE ENGINEERING, CINCINNATI, OHIO/


    Contributors:
    LI, T. Y. (author)

    Published in:

    AIAA Journal ; 5 , 2 ; 233-240


    Publication date :

    1967-01-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English