The aerodynamic characteristics of a thin, cruciform wing consisting of four consoles of arbitrary geometric form are mathematical analyzed.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Cruciform Wing of Finite Span in a Compressible Flow


    Contributors:

    Publication date :

    1963


    Size :

    2 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Finite Span Wings in Compressible Flow

    Krasilschchikova, E A | NTRS | 1956


    Finite span wings in compressible flow

    Krasilshchikova, E.A. | Engineering Index Backfile | 1956


    Wing-wing interference effects for cruciform missiles

    MILLER, M. S. / BURKHALTER, J. E. | AIAA | 1987


    Wing-wing interference effects for cruciform missiles

    MILLER, M. / BURKHALTER, J. | AIAA | 1986