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Comparison of Over-all Impact Loads Obtained During Seaplane Landing Tests with Loads Predicted by Hydrodynamic Theory (1949)

NASA Technical Reports Server (NTRS) · leaf 38

An illustration from Comparison of Over-all Impact Loads Obtained During Seaplane Landing Tests with Loads Predicted by Hydrodynamic Theory, 1949, leaf 38
NACA TN No. 1781 37 … Figure 6.- Installation of amplifying and recording equipment in the main cabin.

NASA Technical Reports Server (NTRS)

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