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Titlebook: Aerodynamics of Tandem Wing Aircraft; From Dinosaurs to UA Illia Kryvokhatko Book 20231st edition The Editor(s) (if applicable) and The Aut

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樓主
發(fā)表于 2025-3-21 17:00:16 | 只看該作者 |倒序?yàn)g覽 |閱讀模式
期刊全稱Aerodynamics of Tandem Wing Aircraft
期刊簡(jiǎn)稱From Dinosaurs to UA
影響因子2023Illia Kryvokhatko
視頻videohttp://file.papertrans.cn/151/150485/150485.mp4
發(fā)行地址?Reviews a wide range of aircraft with four wings, providing insights and best practices.Explains how to choose layout and geometrical parameters of tandem wing aircraft.Maximizes reader understanding
圖書(shū)封面Titlebook: Aerodynamics of Tandem Wing Aircraft; From Dinosaurs to UA Illia Kryvokhatko Book 20231st edition The Editor(s) (if applicable) and The Aut
影響因子This book contains extensive data about tandem wing aircraft. It includes a review of modern flying vehicles with four fixed wings, a review of analytical, numerical and experimental methods; results of the studies about aerodynamics; dependencies between geometrical parameters and aerodynamic characteristics, practical recommendations in development and optimizing of tandem wing aircraft to provide high lift-to-drag ratio, stability, and controllability. This is an ideal book for graduate students, researchers, and engineers working in fields of aerodynamics and conceptual design of the aircraft especially UAVs, ground-effect vehicles, and convertiplanes..?..
Pindex Book 20231st edition
The information of publication is updating

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沙發(fā)
發(fā)表于 2025-3-21 22:38:45 | 只看該作者
板凳
發(fā)表于 2025-3-22 03:02:48 | 只看該作者
,Controlling und Unternehmensführung, increase maximum lift-drag ratio (and therefore flight time), (2) increase maximum lift coefficient (decrease the stalling speed), (3) shift the center of gravity range backward/forward, (4) expand a range of the center of gravity, (5) increase rolling stability, (6) increase directional (yawing) stability.
地板
發(fā)表于 2025-3-22 05:38:54 | 只看該作者
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發(fā)表于 2025-3-22 20:28:05 | 只看該作者
Determination of Tandem Wing Aircraft Aerodynamic Characteristics,g case are discussed. Next, there is a description of a wind tunnel model of a UAV with which multiple tests (weight and visual) were performed. Finally, the comparison of predictions by all the methods is presented including control surface effectiveness with wing-wing interference.
8#
發(fā)表于 2025-3-23 01:02:40 | 只看該作者
Effect of Geometric Parameters on Aerodynamic Characteristics,e degrees of static stability as well. The chapter ends with a CFD study of aerodynamic features of folding design (tube-launched UAV that goes through different sweep angles of the wings immediately after its release).
9#
發(fā)表于 2025-3-23 04:25:51 | 只看該作者
Recommendations Regarding Aerodynamic Design of Tandem Wing Aircraft, increase maximum lift-drag ratio (and therefore flight time), (2) increase maximum lift coefficient (decrease the stalling speed), (3) shift the center of gravity range backward/forward, (4) expand a range of the center of gravity, (5) increase rolling stability, (6) increase directional (yawing) stability.
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發(fā)表于 2025-3-23 09:32:55 | 只看該作者
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