Variation of hydrodynamic impact loads with flight-path angle for prismatic float at 3 degrees trim and with a 22.5 degree angle of dead rise / by Sidney A. Batterson.
Tests were made in the Langley impact basin to determine the relationship between impact normal acceleration and flight-path angle for seaplanes landing on smooth water. The tests were made at both high and low forward speeds with the model at 3 degrees trim. The model had a dead-rise angle of 22.5...
Saved in:
| Main Author: | |
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| Corporate Authors: | , |
| Other title: | NACA Wartime Reports. Series L. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1945]
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| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L211. |
| Subjects: |
Norlin Library - Basement - Government Information - US
| Call Number: |
Y 3.N 21/5:11/L211
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| Y 3.N 21/5:11/L211 | Available Place a Hold |