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Aerodynamic Performance of an Aircraft Equipped with Horizontal Tail Mounted Propellers | Semantic Scholar
![SOLVED: Consider an airplane with the following characteristics Horizontal tail volume ratio:0.38 Tail efficiency:1 Lift slope of the wing airfoil/:0.097 per degree Chord:1m Location of center of gravity of aircraft:0.31 m Location SOLVED: Consider an airplane with the following characteristics Horizontal tail volume ratio:0.38 Tail efficiency:1 Lift slope of the wing airfoil/:0.097 per degree Chord:1m Location of center of gravity of aircraft:0.31 m Location](https://cdn.numerade.com/ask_images/3333a672346646cb8ba8a91a5ba2d8d5.jpg)
SOLVED: Consider an airplane with the following characteristics Horizontal tail volume ratio:0.38 Tail efficiency:1 Lift slope of the wing airfoil/:0.097 per degree Chord:1m Location of center of gravity of aircraft:0.31 m Location
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aircraft design - How are the dimensions of the empennage determined for jetliners? - Aviation Stack Exchange
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