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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