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Transverse Stability of Seaplanes

Transverse Stability of Seaplanes IN a previous article, Twin Float Seaplanes, published in AIRCRAFT ENGINEERING, Vol. V, March 1933, pp. 5456, a typical landplane was taken as an example, which it was desired to fit with notation gear, giving an allup weight of 4,000 lb. as a seaplane. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

Transverse Stability of Seaplanes

Aircraft Engineering and Aerospace Technology , Volume 5 (11): 3 – Nov 1, 1933

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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb029741
Publisher site
See Article on Publisher Site

Abstract

IN a previous article, Twin Float Seaplanes, published in AIRCRAFT ENGINEERING, Vol. V, March 1933, pp. 5456, a typical landplane was taken as an example, which it was desired to fit with notation gear, giving an allup weight of 4,000 lb. as a seaplane.

Journal

Aircraft Engineering and Aerospace TechnologyEmerald Publishing

Published: Nov 1, 1933

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