๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

National advisory committee for aeronautics: Report No. 574. Pressure Distribuion over an airfoil section with a flap and tab: by Carl J. Wenzinger. 11 pages, diagrams, 23 x 29 cms. Washington, Superintendent of Documents, 1936. Price ten cents

Publisher
Elsevier Science
Year
1937
Tongue
English
Weight
68 KB
Volume
223
Category
Article
ISSN
0016-0032

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โœฆ Synopsis

split flaps.

๐Ÿ“œ SIMILAR VOLUMES

Report No. 571, Pressure distribution ov
Report No. 571, Pressure distribution over a rectangular airfoil with a partial-span split flap: by Carl J. Wenzinger and Thomas A. Harris. 12 pages, diagrams, 23.5 ร— 29 cms. Washington, Superintendent of Documents, 1936. Price ten cents
๐Ÿ“‚ Article ๐Ÿ“… 1937 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 60 KB

flow, despite the easy starting, easy scavenging, low mechanical losses, and freedom from knock, renders the quiescent-chamber engine unattractive for aircraft-engine use. P, eport No. 57 I, Pressure Distribution Over a Rectangular Airfoil with a Partial-Span Split Flap, by Carl J. Wenzinger and Tho

National advisory committee for aeronaut
National advisory committee for aeronautics: Report No. 555, Air Flow Around Finned Cylinders, by M. J. Brevoort and Vern G. Rollin. 13 pages, tables, diagrams, 23 ร— 29 curs. Washington, Superintendent of Documents, 1936.Price ten cents
โœ R. ๐Ÿ“‚ Article ๐Ÿ“… 1936 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 60 KB

## BOOK REV1EWS. 243 American Nautical Almanac for I936, which cover all of the problems in the book, and as the methods used in printing the Almanacs are similar in each succeeding year, it can be assured that by mastering the problems for this year, there will be no difficulty in working problem