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Illinois’ SHPE is Regional Chapter of the Year; AE Students Recognized at Convention

The University of Illinois student chapter of the Society of Hispanic Professional Engineers was recognized as the Regional Chapter of the Year, and four Aerospace Engineering undergraduates achieved individual honors during the recent SHPE National Conference.

Lambros Named ASME Fellow

Professor John Lambros makes the third AE faculty member this year to have achieved the status of Fellow within the American Society of Mechanical Engineers (ASME).

Sixty Years and Going Strong

Emeritus Prof. Harry H. Hilton reached a remarkable milestone in September 2009 — his 60th continuous year at the University of Illinois.

College Honors Archambault

The university, college, and Department of Aerospace Engineering welcomed Colonel Lee J. Archambault, BS 82, MS 84 AE, a distinguished United States Air Force pilot and NASA astronaut, back to campus during the Foundation weekend Oct. 2-4.

Events

 

Project 5: Development, evaluation and application of a micro-particle velocimetry system

Adviser(s): Greg Elliott (Associate Professor, Aerospace Engineering)

Project description: In recent years unmanned aerial vehicles (UAVs) have been utilized for surveillance, atmospheric monitoring, payload delivery, and in the program at UIUC to demonstrate principles in aerospace engineering.  Currently, we are seeking a REU student to conduct research designing, building, and testing small reconfigurable mission-flexible UAV concepts.  This will involve utilizing the rapid prototype capabilities at the university to design an aircraft that can be easily reconfigured for the instrumentation and flight profile defined by various mission requirements or in-flight data recorded to determine the aircraft flight characteristics.  For example a fuselage may be designed to incorporate instrumentation such as GPS, flight data collection, telemetry and aerial cameras, but designed so that the wings and control surfaces can be easily reconfigured and optimized for missions requiring loitering, maneuverability, or speed. 

Student background: Although any student interested is encouraged to apply to this project, students who have experience with CAD software packages and/or flying and building radio controlled aircraft are particularly encouraged to apply.

Graph of coefficient of lift versus angle of attack of wing from UAV
   Fig. 1.
Coefficient of lift versus angle of attack of a wing with

and without flaps extended taken from an instrumented UAV.

In-flight video of tufts on UAV investigating attached flow

In-flight video of tufts on UAV investigating attached flow

Fig. 2.  In-flight video recorded of tufts on a UAV investigating attached flow on the wing during level flight and separated flow during stall

 

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