Variation of Hydrodynamic Impact Loads with Flight-Path Angle for Prismatic Float at 3° Trim and With 22 1/2 Angle of Dead Rise. (Restricted Bul L 5A24)
Variation of hydrodynamic impact loads with flight-path angle for prismatic float at 3° trim and with 22 1/2 angle of dead rise
Nat Advisory Committee Aeronautics -- Wartime Report
1945
5 pages
3 Supp plates
Report
Englisch
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Engineering Index Backfile | 1946
|Engineering Index Backfile | 1946
|Engineering Index Backfile | 1947
|Theoretical and experimental dynamic loads for prismatic float having angle of dead rise of 22 1/2°
Engineering Index Backfile | 1945
|Theoretical analysis of hydrodynamic impact of prismatic float having freedom in trim
Engineering Index Backfile | 1952
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