Transverse Stability of Seaplanes

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 November 1933

Abstract

IN a previous article, “Twin Float Seaplanes,” published in AIRCRAFT ENGINEERING, Vol. V, March 1933, pp. 54–56, a typical landplane was taken as an example, which it was desired to fit with notation gear, giving an all‐up weight of 4,000 lb. as a seaplane.

Citation

(1933), "Transverse Stability of Seaplanes", Aircraft Engineering and Aerospace Technology, Vol. 5 No. 11, pp. 271-273. https://doi.org/10.1108/eb029741

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Publisher

:

MCB UP Ltd

Copyright © 1933, MCB UP Limited

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