United States. National Advisory Committee for Aeronautics, United States. National Aeronautics and Space Administration · Washington : G.P.O. · leaf 477
ORY COMMITTEE FOR AERONAUTICS. been already ex])laincd—hocauso for invaria])lc /,/ and tho same altitude, characterized bythe value p^ of the specific load, we read the same speed on the same spewed curve. But allthe other Hying (characteristics vary with the throttle, as can be seen directly from… … the QIP curve is tangent in quadrant I to the lijliy curve (curve in dashes on fig. 19). Atthis throttle opening, the altitude considered is the ceiling. For any smaller throttle opening,the airplane will always be descending. Let us now consider the engine power to be cut off, the airplane can…
Aeronautics
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