MAEWing1: Design, build, test

Chris Regan; Brian R. Taylor

MAEWing1: Design, build, test

Chris Regan
, Brian R. Taylor

Aerospace Engineering and Mechanics

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

28 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 language	English (US)
Title of host publication	AIAA Atmospheric Flight Mechanics Conference
Publisher	American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)	9781624103902
State	Published - 2016
Event	AIAA Atmospheric Flight Mechanics Conference, 2016 - San Diego, United States Duration: Jan 4 2016 → Jan 8 2016

Publication series

Name	AIAA Atmospheric Flight Mechanics Conference

Other

Other	AIAA Atmospheric Flight Mechanics Conference, 2016
Country/Territory	United States
City	San Diego
Period	1/4/16 → 1/8/16

Bibliographical note

Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

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title = "MAEWing1: Design, build, test",

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.",

author = "Chris Regan and Taylor, \{Brian R.\}",

note = "Publisher Copyright: {\textcopyright} 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA Atmospheric Flight Mechanics Conference, 2016 ; Conference date: 04-01-2016 Through 08-01-2016",

year = "2016",

language = "English (US)",

isbn = "9781624103902",

series = "AIAA Atmospheric Flight Mechanics Conference",

publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",

booktitle = "AIAA Atmospheric Flight Mechanics Conference",

}

TY - GEN

T1 - MAEWing1

T2 - AIAA Atmospheric Flight Mechanics Conference, 2016

AU - Regan, Chris

AU - Taylor, Brian R.

PY - 2016

Y1 - 2016

N2 - 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.

AB - 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.

UR - https://www.scopus.com/pages/publications/84958074359

UR - https://www.scopus.com/pages/publications/84958074359#tab=citedBy

M3 - Conference contribution

AN - SCOPUS:84958074359

SN - 9781624103902

T3 - AIAA Atmospheric Flight Mechanics Conference

BT - AIAA Atmospheric Flight Mechanics Conference

PB - American Institute of Aeronautics and Astronautics Inc, AIAA

Y2 - 4 January 2016 through 8 January 2016

ER -

MAEWing1: Design, build, test

Abstract

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