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Propulsion 2 QDR AAE 451: Team 2 Michael Caldwell Jeff Haddin

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Presentation on theme: "Propulsion 2 QDR AAE 451: Team 2 Michael Caldwell Jeff Haddin"— Presentation transcript:

1 Propulsion 2 QDR AAE 451: Team 2 Michael Caldwell Jeff Haddin
Asif Hossain James Kobyra John McKinnis Kathleen Mondino Andrew Rodenbeck Jason Tang Joe Taylor Tyler Wilhelm February 22, 2005

2 Overview 3-View Drawing Thrust Required Power & Endurance Required
Motor & Battery Selection Propeller Selection February 22, 2005

3 Aircraft 3-View Mission Requirements 15 min. endurance
Take-off distance ≤ 60 ft. Vstall ≤ 15 ft./s Vloiter ≤ 25 ft./s 35 ft. turn radius February 22, 2005

4 Thrust Required February 22, 2005

5 Power & Endurance Required
February 22, 2005

6 Motor & Battery Selection
Brushed Brushless February 22, 2005

7 Thrust and Advance Ratio
February 22, 2005

8 Power and Advance Ratio
February 22, 2005

9 Propeller Efficiency and Advance Ratio
February 22, 2005

10 Choice of Motors (RPM) February 22, 2005

11 Propeller Selection Brushless motor propeller Brushed motor propeller
7 in. diameter 3.57 in. pitch 74% efficiency Brushed motor propeller 8 in. diameter 4.59 in. pitch 76% efficiency February 22, 2005

12 Questions? Summary Motor & Battery Selection Propeller Sizing
3 Bladed Props? Questions? February 22, 2005


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