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)
Aircraft performance
Flight
Flight ; 18 , n 8, 12, 17, 21, 25, 30, 34, 43
1926
Article (Journal)
English
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Emerald Group Publishing | 2007
SLUB | 1992
|TIBKAT | 1992
|TIBKAT | 1988
|Engineering Index Backfile | 1930
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