Tests on model to determine relationship between vertical landing acceleration and flight path angle for seaplanes landing in smooth water; results indicated possible hazards accompanying low altitude high speed landings.
Variation of hydrodynamic impact of loads with flight-path angle for prismatic float at 0° and -- 3° trim and with 22 1/2° angle of dead rise
National Advisory Committee Aeronautics -- Technical Note
1947
7 pages
4 Supplementary Plates
Report
English
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Engineering Index Backfile | 1945
|Engineering Index Backfile | 1946
|Engineering Index Backfile | 1946
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