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Titlebook: Aerodynamics of Tandem Wing Aircraft; From Dinosaurs to UA Illia S. Kryvokhatko Book 2025Latest edition The Editor(s) (if applicable) and T

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樓主: hedonist
11#
發(fā)表于 2025-3-23 12:12:45 | 只看該作者
12#
發(fā)表于 2025-3-23 16:05:17 | 只看該作者
13#
發(fā)表于 2025-3-23 18:14:03 | 只看該作者
14#
發(fā)表于 2025-3-24 00:18:42 | 只看該作者
Creating and Maintaining Databasester of gravity range backward/forward, (4) expand a range of the center of gravity, (5) increase rolling stability, (6) increase directional (yawing) stability. The second edition of the book was updated on new studies that were reflected in the recommendations.
15#
發(fā)表于 2025-3-24 05:20:37 | 只看該作者
16#
發(fā)表于 2025-3-24 09:56:13 | 只看該作者
Effect of Geometric Parameters on Aerodynamic Characteristics, different sweep angles of the wings immediately after its release). The second edition is complemented by numerical research on aerodynamic loading where specifics for forward and rear wings due to their interference have been found.
17#
發(fā)表于 2025-3-24 14:00:03 | 只看該作者
Recommendations Regarding Aerodynamic Design of Tandem Wing Aircraft,ter of gravity range backward/forward, (4) expand a range of the center of gravity, (5) increase rolling stability, (6) increase directional (yawing) stability. The second edition of the book was updated on new studies that were reflected in the recommendations.
18#
發(fā)表于 2025-3-24 16:25:11 | 只看該作者
19#
發(fā)表于 2025-3-24 21:35:52 | 只看該作者
Determination of Tandem Wing Aircraft Aerodynamic Characteristics,ical method is presented. Its main advantage over previous theoretical approaches is the possibility to evaluate roll moment, as well as moderate dihedral angles and sweep angles of the wings. Also, it takes into account the contraction of tip vortices to the symmetry plane that improves the accurac
20#
發(fā)表于 2025-3-25 02:52:12 | 只看該作者
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