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Determination of the Stresses Produced by the Landing Impact in the Bulkheads of a Seaplane BottomThe present report deals with the determination of the impact stresses in the bulkhead floors of a seaplane bottom. The dynamic problem is solved on the assumption of a certain elastic system, the floor being assumed as a weightless elastic beam with concentrated masses at the ends (due to the mass of the float) and with a spring which replaces the elastic action of the keel in the center. The distributed load on the floor is that due to the hydrodynamic force acting over a certain portion of the bottom. The pressure distribution over the width of the float is assumed to follow the Wagner law. The formulas given for the maximum bending moment are derived on the assumption that the keel is relatively elastic, in which case it can be shown that at each instant of time the maximum bending moment is at the point of juncture of the floor with the keel. The bending moment at this point is a function of the half width of the wetted surface c and reaches its maximum value when c is approximately equal to b/2 where b is the half width of the float. In general, however, for computing the bending moment the values of the bending moment at the keel for certain values of c are determined and a curve is drawn. The illustrative sample computation gave for the stresses a result approximately equal to that obtained by the conventional factory computation.
Document ID
20050040757
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Memorandum
Authors
Darevsky, V. M.
Date Acquired
September 7, 2013
Publication Date
January 1, 1944
Publication Information
Publication: Report of the Central Aero-Hydrodynamical Inst., Moscow
Subject Category
Aircraft Stability And Control
Report/Patent Number
NACA-TM-1055
Report Number: NACA-TM-1055
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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