A discussion of certain problems connected with the design of hulls of flying boats and the use of general test data (1938)
NASA Technical Reports Server (NTRS) · leaf 6
opted to facilitate comparison of lines. lected arbitrarily to facilitate comparison but it approxi- The adoption of a standard minimum value of A/iZ mates an average value. Equation (13) appears to give free-to-trim at hump speed is also desirable. a reasonable variation in wing loading, while… … '100 200 500 I.OOO 2JXJO 5.000 lODOO presentation are desirable. Wing area, S. sq.fi. 4. The range of loads and speeds necessary to supply Figcbe 5.—Variation of wing loading with gross weight. data for a normal size flying boat appear to be ample to Figure 5 contains a plot of wing loading and…
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