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Report No. 444, Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angels of Attack. VI. Skewed Ailerons on Rectangular Wings: by Fred E. Weick and Joseph A. Shortal, 18 pages, illustrations, 23 × 29 cms. Washington, Superintendent of Documents, 1932. Price five cents

Publisher
Elsevier Science
Year
1932
Tongue
English
Weight
65 KB
Volume
214
Category
Article
ISSN
0016-0032

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✦ Synopsis

Report No. 441, A Flight Investigation of the Spinning of the NY-I Airplane with Varied Mass Distribution and Other Modifications, and an Analysis Based on Wind-Tunnel Tests, by Nathan F

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Report No. 439, Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angels of Attack, V. Spoilers and Ailerons on Rectangular Wings: by Fred E. Weick and Joseph A. Shortal, 18 pages, illustrations, 23 × 29 cms. Washington, Superintendent of Documents, 1932. Price ten cents
📂 Article 📅 1932 🏛 Elsevier Science 🌐 English ⚖ 67 KB

An important result of the measurements is to show that increased aspect ratio gives increased yawing moments for a given area, provided the maximum rudder displacement does not exceed, say, 23 °. If large rudder displacements are used, the effect of aspect ratio is not so great.