Shock expansion method described in Tech Note n 1143, separately indexed, was used to determine principal aerodynamic characteristics of supersonic airfoils; effect of thickness ratio, free stream Mach number, angle of attack, camber, thickness distribution, and aileron deflection; minimum drag of supersonic airfoils obtained when maximum thickness is behind 0.50 chord.


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    Titel :

    Notes on theoretical characteristics of two-dimensional supersonic airfoils


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Ivey, H.R. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    9 pages


    Anmerkungen:

    14 Supp Plates


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Theoretical wave drag and lift of thin supersonic ring airfoils

    Mirels, H. | Engineering Index Backfile | 1948


    Supersonic Channel- Airfoils for Reduced Drag

    Ruffin, S. M. / Gupta, A. / AIAA | British Library Conference Proceedings | 1997


    Thin Oblique Airfoils at Supersonic Speed

    Jones, Robert T | NTRS | 1946