Development of an Improved Model for Aeroelastic Response to Gust Excitation: MARGE-II

Simple item page
dc.contributor.advisorMorgansen, Kristi A
dc.contributor.advisorLivne, Eli
dc.contributor.authorJohnson, Riley Paul
dc.date.accessioned2026-09-16T18:18:40Z
dc.date.issued2026-09-16
dc.date.submitted2026
dc.descriptionThesis (Master's)--University of Washington, 2026
dc.description.abstractThe Model for Aeroelastic Response to Gust Excitation II (MARGE-II) was developed to improve on the existing MARGE-I wind tunnel model’s capabilities to demonstrate and evaluate active control techniques on a flexible aircraft model. The model has been designed for use in the University of Washington’s 3’ x 3’ low-speed wind tunnel located adjacent to the Kirsten Wind Tunnel at the University of Washington. This thesis details the design and fabrication of the model as well as exploratory test results from a tunnel entry in the summer of 2025.
dc.embargo.termsOpen Access
dc.format.mimetypeapplication/pdf
dc.identifier.otherJohnson_washington_0250O_30281.pdf
dc.identifier.urihttps://hdl.handle.net/1773/57679
dc.language.isoen_US
dc.rightsnone
dc.subjectaeroelasticity
dc.subjectgust
dc.subjectwind tunnel
dc.subjectAerospace engineering
dc.subject.otherAeronautics and astronautics
dc.titleDevelopment of an Improved Model for Aeroelastic Response to Gust Excitation: MARGE-II
dc.typeThesis

Files

Original bundle

Now showing 1 - 1 of 1
Thumbnail Image
Name:
Johnson_washington_0250O_30281.pdf
Size:
107.89 MB
Format:
Adobe Portable Document Format
Download

Collections

Aeronautics and astronautics