The impact on floats or hulls during landing as affected by bottom width (1936)
NASA Technical Reports Server (NTRS) · leaf 20
N.A.C.A. Technical Memorandum No. 811 Pigs. 5,6,7,8 t!=0.67|- 0.271 or n=2/3 t - 0.17p _o.l ! J Figure 5.- Half section of float (a) considered in the example … Figure 7.- Impact forces on curved bottoms. §6 n= 2/3I- o.i7|^o.i|3 G-- 6500 kg t= 0.8 o Lmax = 3-76 m v0 = 4. 95 mjs Impact loads not corrected. 1 2 Width B, m Figure 8.- Impact force as function of bottom width for curved bottoms.
NASA Technical Reports Server (NTRS)
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