Price, ten cents. This report contains the results of a series of tests with three wing models. By changing the section of one of the models and painting the surface of another, the number of models tested was increased to five. The tests were made in order to obtain some general information on the
National advisory committee for aeronautics: Report No. 225, The Air Forces on a Model of the Sperry Messenger Airplane without Propeller. By Max M. Munk and Walter S. Diehl. 12 pages, illustrations, quarto. Washington, Government Printing Office, 1925. Price, five cents
- Publisher
- Elsevier Science
- Year
- 1926
- Tongue
- English
- Weight
- 159 KB
- Volume
- 201
- Category
- Article
- ISSN
- 0016-0032
No coin nor oath required. For personal study only.
โฆ Synopsis
Simultaneous equations. V-Non-elemental bases of Tables I andII. VI-Prime numbers less than 5600 (with a = 8n + I, 3, 5 and 7; and some primes greater than 5600). VII-Certain sums of two squares. VIII-Bases of the second kind. IX-Non-elemental bases. X-Summary of certain sums of two squares. XI-Summary of products of two prime numbers. The work is evidently intended for mathematical investigators rather than for those who utilize the results of mathematical research and do not primarily deal with the fundamentals of the subjects. The former type of users will find adequate information in the captions of the tables, but a larger class not so well qualified in the subject, yet deeply interested, would welcome a text on the subject.
However, the tables occupy a fairly large volume and a text might require one as large or larger. The tables, which the author states have been duly checked, represent an immense amount of skilfully directed labor and constitute a valudble addition to the equipment of investigators in the theory of numbers. The press-work is of a high order of excellence.
LUCIEN E. PICOLET.
NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS.. Report No. 225, The Air Forces on a Model of the Sperry Messenger Airplane without Propeller.
๐ SIMILAR VOLUMES
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 fo