Variation of Hydrodynamic Impact Loads with Flight-Path Angle for Prismatic Float at 6° and 9° Trim and 22 1/2° Angle of Dead Rise. (Restricted Bul L5K21)
Variation of hydrodynamic impact loads with flight-path angle for prismatic float at 6° and 9° trim and 22 1/2° angle of dead rise
Nat Advisory Committee Aeronautics -- Wartime Report
1946
6 pages
4 Supp sheets
Report
English
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Engineering Index Backfile | 1945
|Engineering Index Backfile | 1946
|Engineering Index Backfile | 1947
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