Measurement of aerodynamic characteristics of MAVs using motion tracking

Rao, Arjun

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https://hdl.handle.net/2142/30943 Copy

Description

Title

Measurement of aerodynamic characteristics of MAVs using motion tracking

Author(s)

Rao, Arjun

Issue Date

2012-05-22T00:17:27Z

Director of Research (if dissertation) or Advisor (if thesis)

Selig, Michael S.

Department of Study

Aerospace Engineering

Discipline

Aerospace Engineering

Degree Granting Institution

University of Illinois at Urbana-Champaign

Degree Name

M.S.

Degree Level

Thesis

Keyword(s)

• Micro air vehicle (MAV)
• Reynolds number
• remote controlled (RC)
• aircraft
• airplane
• model
• Lift
• drag
• thrust
• moment
• stability
• control
• pitch
• roll
• yaw
• weathercock
• weathervane
• motion tracking
• motion capture
• VICON
• camera
• wand
• Re
• lift curve
• drag polar
• propeller
• Advanced Precision Composites (APC)
• sport
• E-flite
• sideslip
• static margin (SM)
• axis
• axes
• PropellerScanner
• airfoil
• wing
• lifting line theory
• theory
• experimental
• Aerodynamics
• calibration
• noise
• markers
• Euler angles
• longitudinal
• lateral
• advance ratio
• density
• data points
• Extra 260
• Extra 300 3D
• glider
• frequency
• revolutions per minute (RPM)
• body-fixed
• Earth-fixed
• transformation
• rotation
• matrix
• filter
• low-pass
• finite difference
• robust
• lineqar
• least-squares
• parabolic
• Uhlig
• Selig
• Rao

Abstract

Aerodynamic characteristics of Micro Air Vehicles (MAVs) is not well addressed in aeronautics literature, and more experimental data are required to help better understand the behavior of fixed-wing MAVs. In the current research, aerodynamic and stability characteristics of two MAVs were measured using a motion tracking system. Both the aircraft position and propeller rotation were tracked. The aircraft used were flat foam surface, highly aerobatic RC models. Tests were conducted for unpowered and powered flight conditions to assess the aerodynamic performance of a commercially manufactured Extra 300 3D and a custom-built Extra 260 with wingspans of 42.67 cm (16.8 in) and 41.27 cm (16.25 in), respectively. A comparison of theoretical calculations with experimental results was made for parameters such as the lift curve and neutral point location. The aircraft used in this research operated in a Reynolds number range of 20,000 to 30,000. Low Reynolds numbers effects that influence the aerodynamic characteristics and performance of the aircraft are discussed in this thesis. The behavior of MAVs in powered flight was analyzed by testing the Extra 300 3D over a range of propeller advance ratios (J = 0.3–1.0) with the propeller running at pre-determined speeds (RPM). A thrust model was developed for a commercially manufactured propeller, and the lift and drag characteristics of the aircraft was analyzed. The results indicate that the propeller induced flow influences the aerodynamic performance of the aircraft. Results indicate a delay in the onset of stall, an increase in the lift curve slope, and reduction in drag with decreasing advance ratios (J). The results show a myriad of interesting aerodynamic trends that are discussed.

Graduation Semester

2012-05

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http://hdl.handle.net/2142/30943

Copyright and License Information

Copyright 2012 by Arjun Harsha Rao. All rights reserved.

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