Smooth water step landing of seaplane is analyzed by solving Newton's differential equation of motion entailing reasonable limiting assumptions; formulas are developed for maximum acceleration; solution is dependent upon definition of apparent water mass.
Impact theory for seaplane landings
National Advisory Committee Aeronautics -- Technical Note
1947
52 pages
Report
English
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Impact theory for seaplane landings
NTRS | 1947
|Impact theory for seaplane landings
TIBKAT | 1947
|Engineering Index Backfile | 1949
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