Published October 1929 | Version Published
Technical Report Open

The impact on seaplane floats during landing

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.

Additional Information

No Copyright.

Attached Files

Published - KARnacatn321.pdf

Files

KARnacatn321.pdf

Files (248.8 kB)

Name Size Download all
md5:561e178a02f097b9c34f3b78359486f4
248.8 kB Preview Download

Additional details

Identifiers

Eprint ID
47898
Resolver ID
CaltechAUTHORS:20140804-120956389

Related works

Dates

Created
2014-08-04
Created from EPrint's datestamp field
Updated
2019-10-03
Created from EPrint's last_modified field

Caltech Custom Metadata

Other Numbering System Name
NACA Technical Note
Other Numbering System Identifier
321