Date

5-6-2019

Document Type

Thesis

Abstract

This project designs aircraft that addresses the space constraint that limits airport capacity by exploiting lift created by flying aircraft at high speeds (350-500KIAS) in the mid altitudes of FL100-FL200 to increase the payload of smaller aircraft. Three solutions with the length and wingspan footprint of the Boeing 737-800 are produced using the software X-Plane, then virtually flight tested for various performance data. The results find that adoption of these designs can yield significant capacity increases, albeit at reduced fuel efficiency.

Department

Aviation Science

Thesis Comittee

Prof. Veronica Cote, Thesis Advisor

Prof. Michael Farley, Committee Member

Prof. Michael Welch, Committee Member

Copyright and Permissions

Original document was submitted as an Honors Program requirement. Copyright is held by the author.

Included in

Aviation Commons

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