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Estimation of Hydrodynamic Impact Loads and Pressure Distributions on Bodies Approximating Elliptical Cylinders with Special Reference to Water Landings of HelicoptersAn approximate method for computing water loads and pressure distributions on lightly loaded elliptical cylinders during oblique water impacts is presented. The method is of special interest for the case of emergency water landings of helicopters. This method makes use of theory developed and checked for landing impacts of seaplanes having bottom cross sections of V and scalloped contours. An illustrative example is given to show typical results obtained from the use of the proposed method of computation. The accuracy of the approximate method was evaluated through comparison with limited experimental data for two-dimensional drops of a rigid circular cylinder at a trim of 0 degrees and a flight -path angle of 90 degrees. The applicability of the proposed formulas to the design of rigid hulls is indicated by the rough agreement obtained between the computed and experimental results. A detailed computational procedure is included as an appendix.
Document ID
19930083799
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Schnitzer, Emanuel
Hathaway, Melvin E
Date Acquired
September 6, 2013
Publication Date
April 1, 1953
Report/Patent Number
NACA-TN-2889
Report Number: NACA-TN-2889
Accession Number
93R13089
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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