Variation of Hydrodynamic Impact Loads With Flight-Path Angle for a Prismatic Float at 3 Degree Trim and With a 22 1/2 Degree Angle of Dead Rise

Author: Batterson, Sidney A.
Year: 1945
Document Type: N/A
Series: NACA Wartime Reports
Report Number: NACA-WR-L-211, NACA-RB-L5A24
Link: https://digital.library.unt.edu/ark:/67531/metadc61796/

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