Feb 25 1926 n 8 p 110a-110c: Indicated air speed for given true air speed and height; lift coefficient forgiven indicated air speed and loading. Mar 25 1926 n 12 p 178c-178f: Wing sections in light of vortex theory. Apr 29 1926 n 17 p 260d-260g: Wing proportions in light of vortex theory. May 27 1926 n 21 p 308e-308g: Scale effect. June 24 1926 n 25 p 362a-362d: Causes of drag; possible improvements in design and high loading. July 29 1926 n 30 p 464e-464g: Influence of size on structure weight. Aug 26 1926 n 34 p 532a-532e and Oct 28 1926 n 43 p 702a-702d: Structural policy in design. (Aircraft Engr.) (See also - no. 47 Nov. 25 1926, pp. 764e-764g; vol. 19, nos. 4, 13, 21, 25, Jan. 27, Mar. 31, May 26, and June 23, 1927, pp. 46e-46f, 188a-188c, 330a-330b and 414a-414c)


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    Title :

    Aircraft performance


    Additional title:

    Flight


    Contributors:
    North, J.D. (author)

    Published in:

    Flight ; 18 , n 8, 12, 17, 21, 25, 30, 34, 43


    Publication date :

    1926


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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