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The impact on seaplane floats during landingIn 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.
Document ID
19930081174
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Von Karman, TH
(Aerodynamical Institute of the Technical High School, Aachen)
Date Acquired
September 6, 2013
Publication Date
October 1, 1929
Report/Patent Number
NACA-TN-321
Report Number: NACA-TN-321
Accession Number
93R10464
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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