THE wind tunnel, through the use of models, offers a convenient means of investigating the aerodynamic characteristics of various parts of the aeroplane, individually or as a unit, and results obtained in it are generally applicable, within the limits of engineering precision, for the purpose of estimating full-scale performance. It is believed that the results of control surface tests on models may be taken to represent full-scale conditions with approximately the same degree of precision.
Control by Conventional Ailerons
Results of a Series of Wind-Tunnel Experiments Carried out by the U.S. Bureau of Standards
Aircraft Engineering and Aerospace Technology ; 3 , 12 ; 315-318
1931-12-01
4 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Engineering Index Backfile | 1938
|Control of airplanes at low speeds by means of conventional ailerons
Engineering Index Backfile | 1931
Engineering Index Backfile | 1932
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