Progress Report - March 29

Progress Report - March 29 - Wind Tunnel Testing AAE 520...

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AAE 520 – Final Project Experimental Assessment of the Aerodynamic Performance of Numerically Optimized Rotor-blade Airfoils David Fanjoy Eddie Pérez-Ruberté
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AAE 520 – Final Project FS-GA1 Result of a shape design procedure with a Genetic Algorithm Aerodynamic analysis from a panel code with integral boundary layer scheme Optimized for drag subject to lift and pitching moment constraints
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AAE 520 – Final Project Overview Model construction Planned dimensions: AR = 6 Chord: c = 10 in. Span: b = 5 ft. (60 in.) Design manufacturing procedures Wooden ribs and spars CNC procedure for ribs “wing-jig” Thin skin Ease of handling Design pressure-tap fixture (underway)
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Unformatted text preview: Wind Tunnel Testing AAE 520 Final Project Model construction Ribs Spars AAE 520 Final Project Milestone Forecast (Gantt Chart) 19 20 21 22 23 24 25 26 27 28 29 30 31 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 S M T W T F S S M T W T F S S M T W T F S S M T W T F S S M T W T F S S M T W T F S S Decide Airfoil 3/20/00 Research on Building 3/21/00 Sullivan/Build/Materials 3/27/00 Design Model 3/28/00 Progress Report 3/29/00 Build Model 4/3/00 Progress Report 4/5/00 Wind Tunnel Testing 4/9/00 Progress Report 4/12/00 Data Analysis 4/16/00 Progress Report 4/19/00 Final Report Composing 4/23/00 Projected Actual March April Tasks Start...
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This note was uploaded on 01/15/2012 for the course AAE 490 taught by Professor Andrisani during the Fall '09 term at Purdue University-West Lafayette.

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Progress Report - March 29 - Wind Tunnel Testing AAE 520...

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