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 1
t-hand angle of trim may lead to erroneous conclusions. Un- side of figure 3 locates the values of Ca, Ct-1, and A/R at fortunately, the tests. in reference 3 do not cover the hump. This curve can be drawn alone on a sepa- enough range in trim angles and loadings to illustrate rate chart as on… … .C .J .■v Constant angle unloading is shown on tliis plot by a Load coefficient of hump, straight line drawn from the initial load coefficient Figuhe 2.—Variation of AIR and maximum trim angle at hump for model 110 Ca0 to the get-away value of Cv*. An example of this (based on data from reference…
NASA Technical Reports Server (NTRS)
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