Full scale drag tests on various parts of Sperry Messenger airplane

Book details

Title
Full scale drag tests on various parts of Sperry Messenger airplane
Publication year listed
1928
Format
Public domain eBook
Reading access
Free online reader; no registration required
Source record
View on Archive.org

About this book

Full scale drag tests on various parts of Sperry Messenger airplane

Author: Weick, Fred

Year: 1928

The drag of a Sperry Messenger airplane with the wings removed, and also the drag of its various component parts, was measured in the 20-foot air stream of the N.A.C.A. propeller research tunnel at air speeds from 50 to 100 m.p.h. It was found that the three-cylinder radial air-cooled engine nearly doubled the drag of the bare fuselage, and the drag of the landing gear was about the same as that of the fuselage and engine combined.

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