Fuctionary
发表于 2025-3-21 17:00:16
书目名称Aerodynamics of Tandem Wing Aircraft影响因子(影响力)<br> http://figure.impactfactor.cn/if/?ISSN=BK0150485<br><br> <br><br>书目名称Aerodynamics of Tandem Wing Aircraft影响因子(影响力)学科排名<br> http://figure.impactfactor.cn/ifr/?ISSN=BK0150485<br><br> <br><br>书目名称Aerodynamics of Tandem Wing Aircraft网络公开度<br> http://figure.impactfactor.cn/at/?ISSN=BK0150485<br><br> <br><br>书目名称Aerodynamics of Tandem Wing Aircraft网络公开度学科排名<br> http://figure.impactfactor.cn/atr/?ISSN=BK0150485<br><br> <br><br>书目名称Aerodynamics of Tandem Wing Aircraft被引频次<br> http://figure.impactfactor.cn/tc/?ISSN=BK0150485<br><br> <br><br>书目名称Aerodynamics of Tandem Wing Aircraft被引频次学科排名<br> http://figure.impactfactor.cn/tcr/?ISSN=BK0150485<br><br> <br><br>书目名称Aerodynamics of Tandem Wing Aircraft年度引用<br> http://figure.impactfactor.cn/ii/?ISSN=BK0150485<br><br> <br><br>书目名称Aerodynamics of Tandem Wing Aircraft年度引用学科排名<br> http://figure.impactfactor.cn/iir/?ISSN=BK0150485<br><br> <br><br>书目名称Aerodynamics of Tandem Wing Aircraft读者反馈<br> http://figure.impactfactor.cn/5y/?ISSN=BK0150485<br><br> <br><br>书目名称Aerodynamics of Tandem Wing Aircraft读者反馈学科排名<br> http://figure.impactfactor.cn/5yr/?ISSN=BK0150485<br><br> <br><br>
Vertical
发表于 2025-3-21 22:38:45
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确定无疑
发表于 2025-3-22 03:02:48
,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.
botany
发表于 2025-3-22 05:38:54
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Ankylo-
发表于 2025-3-22 09:46:35
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capsaicin
发表于 2025-3-22 14:20:45
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星星
发表于 2025-3-22 20:28:05
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.
减少
发表于 2025-3-23 01:02:40
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).
富饶
发表于 2025-3-23 04:25:51
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.
adduction
发表于 2025-3-23 09:32:55
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