MAEWing1: Design, build, test

Chris Regan, Brian R. Taylor

Research output: Chapter in Book/Report/Conference proceedingConference contribution

14 Scopus citations

Abstract

The design, build, and testing of a flexible, flying wing aircraft, the mAEWing1, has been accomplished with an emphasis on a research-through-development approach. Design goals of the mAEWing1 aircraft, including structural sizing and systems selection are addressed. An overview of the aircraft construction and integration are included. Testing methodology and test results, including nominal values and estimated uncertainty, are presented at a high level.

Original languageEnglish (US)
Title of host publicationAIAA Atmospheric Flight Mechanics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624103902
StatePublished - 2016
EventAIAA Atmospheric Flight Mechanics Conference, 2016 - San Diego, United States
Duration: Jan 4 2016Jan 8 2016

Publication series

NameAIAA Atmospheric Flight Mechanics Conference

Other

OtherAIAA Atmospheric Flight Mechanics Conference, 2016
CountryUnited States
CitySan Diego
Period1/4/161/8/16

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