✦ LIBER ✦

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

Publisher: Elsevier Science
Year: 1932
Tongue: English
Weight: 67 KB
Volume: 214
Category: Article
ISSN: 0016-0032
DOI: 10.1016/s0016-0032(32)91220-4

No coin nor oath required. For personal study only.

✦ Synopsis

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.

📜 SIMILAR VOLUMES

Report No. 444, Wind-Tunnel Research Com

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

📂 Article 📅 1932 🏛 Elsevier Science 🌐 English ⚖ 65 KB

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

National advisory committee for aeronaut

National advisory committee for aeronautics: Report No. 424, Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. IV. Floating tip ailerons on rectangular wings: by Fred E. Weick and Thomas A. Harris, 25 pages, illustrations, 23 × 29 cms. Washington, Superintendent of Documents, 1932, price ten cents

📂 Article 📅 1932 🏛 Elsevier Science 🌐 English ⚖ 125 KB

Report no. 510, wind-tunnel research com

Report no. 510, wind-tunnel research comparing lateral control devices particularly at high angles of attack. XIII—Auxiliary airfoils used as external ailerons: by Fred E. Weick and Richard W. Noyes. 32 pages, tables, illustrations, 23.5 × 29 cms.Washington, Superintendent of Documents, 1935. Price ten cents

📂 Article 📅 1935 🏛 Elsevier Science 🌐 English ⚖ 80 KB

Report No. 423, Wind-tunnel research com

Report No. 423, Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. III. Ordinary ailerons rigged up 10° when neutral: by Fred E. Weick and Carl J. Wenzinger, 12 pages, illustrations, 23 × 29 cms. Washington, Superintendent of Documents, 1932

📂 Article 📅 1932 🏛 Elsevier Science 🌐 English ⚖ 87 KB

National advisory committee for aeronaut

National advisory committee for aeronautics: Report No. 422, Wind-tunnel Research comparing lateral control devices, particularly at hgh angles of attack. II. Slotted ailoerons, and frise Ailerons, by Fred E. Weick and Richard W. Noyes, 16 pages, illustrations, 23 × 29 cms. Washington, Superintendent of Documents, 1932

📂 Article 📅 1932 🏛 Elsevier Science 🌐 English ⚖ 87 KB

National advisory committee for aeronaut

National advisory committee for aeronautics: Report No. 428, Wind-tunnel tests of a clark Y wing with a narrow auxiliary airfoil in different positions: by Fred E. Weick and Millard J. Bamber, 14 pages, illustrations, 23 × 29 cms. Washington, Superintendent of Documents, 1932, price ten cents

📂 Article 📅 1932 🏛 Elsevier Science 🌐 English ⚖ 64 KB