✦ LIBER ✦

Report No. 357. Aircraft accidents—Methods of analysis: Report prepared by Committee on Aircraft Accidents. 17 pages, illustrations, quarto. Washington, Government Printing Office, 1930. Price ten cents

Book ID: 108320786
Publisher: Elsevier Science
Year: 1930
Tongue: English
Weight: 77 KB
Volume: 210
Category: Article
ISSN: 0016-0032
DOI: 10.1016/s0016-0032(30)90273-6

No coin nor oath required. For personal study only.

📜 SIMILAR VOLUMES

Report No. 308. Aircraft accidents metho

Report No. 308. Aircraft accidents method of analysis: Report prepared by Special Committee on the Nomenclature, Subdivision, and Classification of Aircraft Accidents. 18 pages, illustrations, quarto. Washington, Government Printing Office, 1928, price, ten cents

📂 Article 📅 1928 🏛 Elsevier Science 🌐 English ⚖ 123 KB

National advisory committee for aeronaut

National advisory committee for aeronautics. Report No. 576, aircraft accidents—Methods of analysis, report prepared by committee on aircraft accidents: 10 pages, diagrams, 23 × 29 cms. Washington, Superintendent of Documents, 1936. Price ten cents

📂 Article 📅 1936 🏛 Elsevier Science 🌐 English ⚖ 124 KB

Report No. 299. Investigation of damping

Report No. 299. Investigation of damping liquids for aircraft instruments: by G. H. Keulegan. 24 pages, illustrations, quarto. Washington, Government Printing Office, 1929. Price, ten cents

📂 Article 📅 1929 🏛 Elsevier Science 🌐 English ⚖ 58 KB

Report No. 354. Aircraft woods: Their pr

Report No. 354. Aircraft woods: Their properties, selection and characteristics: by L. J. Markwardt. 34 pages, illustrations, quarto. Washington, Government Printing Office, 1930. Price twenty cents

📂 Article 📅 1930 🏛 Elsevier Science 🌐 English ⚖ 121 KB

Report no. 344. The design of plywood we

Report no. 344. The design of plywood webs for airplane wing beams: By George W. Trayer. 17 pages, illustrations, quarto. Washington, Government Printing Office, 1930. Price ten cents

📂 Article 📅 1930 🏛 Elsevier Science 🌐 English ⚖ 66 KB

The measurements were made at various angles of pitch but at zero angle of roll and yaw, the wing chord being set at an angle of + 4 ° to, the fuselage axis. In the case of the Clark Y airfoil the measurements have been extended to a pitch angle of 4 o°, using ailerons of span equal to 67 per cent.

Report no. 346. Water pressure distribut

Report no. 346. Water pressure distribution on a flying boat hull: By F. L. Thompson. 18 pages, illustrations, quarto. Washington, Government Printing Office, 1930. Price ten cents

📂 Article 📅 1930 🏛 Elsevier Science 🌐 English ⚖ 135 KB