248 REPORT NO. 65^-NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS … Figure 6.—The quantity Clt as a function of A. airplane is indicated as T-Ve. The value of this speed 500 will depend, for given thrust power-required char- acteristics, on the slope of the power-available curve, which in turn will depend upon the particular engine- 400 propeller combination and…
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