𝔖 Bobbio Scriptorium
✦   LIBER   ✦

National advisory committee for aeronautics: Report No. 657, The Influence of Directed Air Flow on Combustion in a Spark-Ignition Engine, by A. M. Rothrock and R. C. Spencer. 14 pages, illustrations, tables, 23 × 29 CMS. Washington, Government Printing Office, 1939.Price 10 cents

Publisher
Elsevier Science
Year
1939
Tongue
English
Weight
150 KB
Volume
228
Category
Article
ISSN
0016-0032

No coin nor oath required. For personal study only.

✦ Synopsis

within the range investigated because stalling, in general, did not occur.

Sections for fixed-pitch propellers should be selected on a basis of both minimum drag and maximum lift, particularly for blade-angle settings of 20' and over, because the take-off thrust power increased with maximum lift for the higher blade angles. Report No. 655, The Knocking Characteristics of Fuels in Relation to Maximum Permissible Performance of Aircraft Engines, by _A. M. Rothrock and Arnold E. Biermann. 22 pages, illustrations, tables, 23 X 29 ems. Washington, Government Printing Office, 1939. Price I0 cents.

📜 SIMILAR VOLUMES

National advisory committee for aeronaut
National advisory committee for aeronautics: Report No. 656, The Column Strength of Two Extruded Aluminum-Alloy H-Sections, by William R. Osgood and Marshall Holt. 26 pages, illustrations, tables, 23 × 29 CMS. Washington, Government Printing Office, 1939. Price 10 cents
📂 Article 📅 1939 🏛 Elsevier Science 🌐 English ⚖ 77 KB

J. 1;. I. within the range investigated because stalling, in general, did not occur. Sections for fixed-pitch propellers should be selected on a basis of both minimum drag and maximum lift, particularly for blade-angle settings of 20' and over, because the take-off thrust power increased with maxim