No 391: 43 series with maximum mean camber of 4 per cent of chord at position 0.3 of chord from leading edge; 63 series with maximum mean camber of 6 per cent of chord at same position; variation of aerodynamic characteristics with profile thickness for airfoils having certain mean camber line. No. 392: 45 series, has maximum mean camber of 4 per cent of chord at position 0.5 of chord behind loading edge; 65 series, has maximum mean camber of 6 per cent of chord at same position; maximum thickness-chord ratios being: 0.06, 0.09, 0.12, 0.15, 0.18 and 0.21.


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    Title :

    Tests of N.A.C.A. Airfoils in variable-density wind tunnel, series 4e and 63


    Additional title:

    Nat. Advisory Committee Aeronautics -- Tech. Notes


    Contributors:


    Publication date :

    1931


    Size :

    32 pages


    Remarks:

    11, 12 figs on supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Tests of N.A.C.A. airfoils in variable-density wind tunnel, series 24

    Jacobs, E.N. / Ward, K.E. | Engineering Index Backfile | 1932


    Tests of N.A.C.A. Airfoils in variable-density wind tunnel

    Jacobs, E.N. / Pinkerton, R.M. | Engineering Index Backfile | 1936



    Tests of N.A.C.A. airfoils in the variable-density wind tunnel Series 230.

    Jacobs, Eastman N / Pinkerton, Robert M | NTRS | 1936


    Tests of N.A.C.A. airfoils in the variable-density wind tunnel ; 5: Series 24

    Jacobs, Eastman N. / Ward, Kenneth E. | TIBKAT | 1931