Application of modified hydrodynamic theory for landing impact of seaplane floats. (Restricted Bul L5F15)
Theoretical and experimental dynamic loads for prismatic float having angle of dead rise of 22 1/2°
Nat Advisory Committee Aeronautics -- Wartime Report
1945
11 pages
4 Supp plates
Report
Englisch
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Engineering Index Backfile | 1945
|Engineering Index Backfile | 1946
|Engineering Index Backfile | 1946
|Engineering Index Backfile | 1947
|Theoretical analysis of hydrodynamic impact of prismatic float having freedom in trim
Engineering Index Backfile | 1952
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