1 / 7

“Very Light” Wing Billet Thermal Analysis

“Very Light” Wing Billet Thermal Analysis. Brad Allen, Joseph Ashby, Aaron Worlton ME 340 Fall 2006. Disclaimer:. This information is not public information. The analysis is based off a Spectrum Aeronautical airplane design, and should not be used without their consent. Thank you.

Download Presentation

“Very Light” Wing Billet Thermal Analysis

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


  1. “Very Light” Wing Billet Thermal Analysis Brad Allen, Joseph Ashby, Aaron Worlton ME 340 Fall 2006

  2. Disclaimer: • This information is not public information. The analysis is based off a Spectrum Aeronautical airplane design, and should not be used without their consent. Thank you.

  3. The Problem • Find all nodal temperatures during the heating of a aluminum wing billet. • How many heating elements are needed to obtain 450 K at the center of wing billet?

  4. Assumptions: • The billet shape is symmetrical. • EGC Enterprises Q Foil Heaters were used as the heating elements. • Heaters Produce q’’ = 100 W/in^2 • (q_dot = 2.44x10^8 W/m^3) • Forced air convection • Heaters only cover the top and bottom of wing billet.

  5. The Break-Down

  6. Temperature Profile

  7. Conclusions • All nodal temperatures were found. • 450 K was obtained at the center of wing billet. • 2880 – 1in^2 heaters needed.

More Related