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Variation of Hydrodynamic Impact Loads With Flight-Path Angle for a Prismatic Float at 0 and -3 Degree Trim and With a 22 1/2 Degree Angle of Dead Rise
Author:
Batterson, Sidney A.
Year:
1947
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-1166
Link:
https://digital.library.unt.edu/ark:/67531/metadc55226/
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