2006
DOI: 10.1007/bf02916487
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Aerodynamic analysis of tilt-rotor Unmanned Aerial Vehicle with computational fluid dynamics

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Cited by 15 publications
(2 citation statements)
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“…The airflow domain, as shown in Figure 4, was built around both Neo-Ptero models according to the total chordwise aircraft length (C = 594.5 mm) as proposed by [9,10]. Only half of the airflow domain and the Neo-Ptero models were implemented in the virtual wind tunnel analysis to avoid computational burden [11].…”
Section: Airflow Domain and Mesh Generationmentioning
confidence: 99%
“…The airflow domain, as shown in Figure 4, was built around both Neo-Ptero models according to the total chordwise aircraft length (C = 594.5 mm) as proposed by [9,10]. Only half of the airflow domain and the Neo-Ptero models were implemented in the virtual wind tunnel analysis to avoid computational burden [11].…”
Section: Airflow Domain and Mesh Generationmentioning
confidence: 99%
“…Research shows that fuel consumption will be reduced by 7percent to 9percent if the aerodynamic drag coefficient is reduced by 20percent for a medium duty van when traveling at 80Km/h [1]. Therefore, reducing the aerodynamic drag of vehicle when driving plays a significant role in energy saving, emission reducing and environment protecting [2][3][4].…”
Section: Introductionmentioning
confidence: 99%