The Effect of Tip Clearance on Performance of a Counter-Rotating Ducted Fan in a VTOL UAV

This research analyzed the effect of tip clearance on counter-rotating ducted fans for vertical take-off and landing in unmanned aerial vehicles using commercial computational fluid dynamics tools. The computational results were verified using the subsonic wind tunnel at Hanyang University. In this...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Veröffentlicht in:	TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 2017, Vol.60(1), pp.1-9
Hauptverfasser:	RYU, Minhyoung, CHO, Leesang, CHO, Jinsoo
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics CFD Computational fluid dynamics Counter-Rotating Ducted Fan Ducted fans Fluid flow Leakage Mass flow rate Rotation Rotors Software Subsonic aircraft Subsonic wind tunnels Tip Clearance Unmanned aerial vehicles Vertical landing Wind Tunnel Test Wing tip vortices
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Schreiben Sie den ersten Kommentar!