For high-altitude piston engines, for instance, the curve for the relation VmnT = f( H) has the peculiar form a) 3000 2500 2000 ISOO 1000 500 HJO 200 300 m 500 600 b) Fig. ... This curve has two local maxima corresponding to the two limits of the altitude performance of the engine (or other number of ... IV) The excess power for each speed and flight altitude is determined directly from the power diagram.

Title | : | Aircraft aerodynamics |

Author | : | I. V. Ostoslavskiĭ |

Publisher | : | - 1957 |

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