Comparison of Over-all Impact Loads Obtained During Seaplane Landing Tests with Loads Predicted by Hydrodynamic Theory (1949)
NASA Technical Reports Server (NTRS) · leaf 45
10 r It ft k … NACA TN No. 1781 (h) Run 20: Vv = 6.3 feet per second; (g) Run 18: V = 6.5 feet per second; vo Vv, = 94 feet per second; u)n = -2.6 = 102 feet per second; u0 = -4.2 IJo u degrees per second. degrees per second. Figure 9.- Continued.
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