“Very Light” Wing Billet Thermal Analysis
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Transcript of “Very Light” Wing Billet Thermal Analysis
““Very Light” Wing Billet Very Light” Wing Billet Thermal AnalysisThermal Analysis
Brad Allen, Joseph Ashby, Brad Allen, Joseph Ashby,
Aaron WorltonAaron WorltonME 340 Fall 2006ME 340 Fall 2006
Disclaimer:Disclaimer:
This information is not public This information is not public information. The analysis is based information. The analysis is based off a Spectrum Aeronautical airplane off a Spectrum Aeronautical airplane design, and should not be used design, and should not be used without their consent. Thank you.without their consent. Thank you.
The ProblemThe Problem
Find all nodal temperatures during Find all nodal temperatures during the heating of a aluminum wing the heating of a aluminum wing billet.billet.
How many heating elements are How many heating elements are needed to obtain 450 K at the center needed to obtain 450 K at the center of wing billet?of wing billet?
Assumptions:Assumptions:
The billet shape is symmetrical.The billet shape is symmetrical. EGC Enterprises Q Foil Heaters were EGC Enterprises Q Foil Heaters were
used as the heating elements.used as the heating elements. Heaters Produce q’’ = 100 W/in^2 Heaters Produce q’’ = 100 W/in^2
(q_dot = 2.44x10^8 W/m^3)(q_dot = 2.44x10^8 W/m^3) Forced air convectionForced air convection Heaters only cover the top and bottom Heaters only cover the top and bottom
of wing billet.of wing billet.
The Break-DownThe Break-Down
Temperature ProfileTemperature Profile
ConclusionsConclusions
All nodal temperatures were found.All nodal temperatures were found. 450 K was obtained at the 450 K was obtained at the
center of wing billet.center of wing billet. 2880 – 1in^2 heaters needed.2880 – 1in^2 heaters needed.