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The impact on seaplane floats during landing

von Kármán, Th. (1929) The impact on seaplane floats during landing. National Advisory Committee on Aeronautics , Washington, DC. https://resolver.caltech.edu/CaltechAUTHORS:20140804-120956389

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Abstract

In order to make a stress analysis of seaplane floats, and especially of the members connecting the floats with the fuselage, it is of great importance to determine the maximum pressure acting on the floats during landing. Here, the author gives a formula for maximum pressures during landing that permits one to apply experimental results to different bodies and different velocities. The author notes that the formula checks very well with experimental results.


Item Type:Report or Paper (Technical Report)
Related URLs:
URLURL TypeDescription
http://hdl.handle.net/2060/19930081174OrganizationArticle
Additional Information:No Copyright.
Other Numbering System:
Other Numbering System NameOther Numbering System ID
NACA Technical Note321
Record Number:CaltechAUTHORS:20140804-120956389
Persistent URL:https://resolver.caltech.edu/CaltechAUTHORS:20140804-120956389
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:47898
Collection:CaltechAUTHORS
Deposited By: George Porter
Deposited On:04 Aug 2014 20:03
Last Modified:03 Oct 2019 06:58

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