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Variation of hydrodynamic impact loads with flight-path angle for a prismatic float at 6 degrees and 9 degrees trim and a 22-1/2 degree angle of dead rise
Document ID
19930093046
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Stewart, Thelma
Date Acquired
August 16, 2013
Publication Date
February 1, 1946
Report/Patent Number
NACA-WR-L-69
NACA-RB-L5K21
Report Number: NACA-WR-L-69
Report Number: NACA-RB-L5K21
Accession Number
93R22336
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLOATS - IMPACT - TANK TESTS (NACA)
LANDINGS - SEAPLANES
LOADS - FLOATS

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