mAEWing2: Conceptual design and system test

Christopher D. Regan

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

28 Scopus citations

Abstract

The conceptual design, build plan, and test plan of a flexible, flying wing aircraft, the mAEWing2, has been accomplished. mAEWing2 is a 50% scaled aircraft based on the X-56A aircraft. The aircraft has been developed as an incremental step in technology application and test method development. Design goals and high-level requirements of the mAEWing2 aircraft, including determination and specification of flight performance, structural sizing, and flight system specifications are addressed. An overview of the aircraft build and test plans are included.

Original languageEnglish (US)
Title of host publicationAIAA Atmospheric Flight Mechanics Conference, 2017
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624104480
DOIs
StatePublished - 2017
EventAIAA Atmospheric Flight Mechanics Conference, 2017 - Denver, United States
Duration: Jun 5 2017Jun 9 2017

Publication series

NameAIAA Atmospheric Flight Mechanics Conference, 2017

Other

OtherAIAA Atmospheric Flight Mechanics Conference, 2017
Country/TerritoryUnited States
CityDenver
Period6/5/176/9/17

Bibliographical note

Publisher Copyright:
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

Fingerprint

Dive into the research topics of 'mAEWing2: Conceptual design and system test'. Together they form a unique fingerprint.

Cite this