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

Fuctionary

書(shū)目名稱(chēng)Aerodynamics of Tandem Wing Aircraft影響因子(影響力)




書(shū)目名稱(chēng)Aerodynamics of Tandem Wing Aircraft影響因子(影響力)學(xué)科排名




書(shū)目名稱(chēng)Aerodynamics of Tandem Wing Aircraft網(wǎng)絡(luò)公開(kāi)度




書(shū)目名稱(chēng)Aerodynamics of Tandem Wing Aircraft網(wǎng)絡(luò)公開(kāi)度學(xué)科排名




書(shū)目名稱(chēng)Aerodynamics of Tandem Wing Aircraft被引頻次




書(shū)目名稱(chēng)Aerodynamics of Tandem Wing Aircraft被引頻次學(xué)科排名




書(shū)目名稱(chēng)Aerodynamics of Tandem Wing Aircraft年度引用




書(shū)目名稱(chēng)Aerodynamics of Tandem Wing Aircraft年度引用學(xué)科排名




書(shū)目名稱(chēng)Aerodynamics of Tandem Wing Aircraft讀者反饋




書(shū)目名稱(chēng)Aerodynamics of Tandem Wing Aircraft讀者反饋學(xué)科排名

Vertical

確定無(wú)疑

,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.

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星星

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.

減少

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).

富饒

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