Between Dec 19, 2024 and Jan 2, 2025, datasets can be submitted to DRUM but will not be processed until after the break. Staff will not be available to answer email during this period, and will not be able to provide DOIs until after Jan 2. If you are in need of a DOI during this period, consider Dryad or OpenICPSR. Submission responses to the UDC may also be delayed during this time.
 

mAEWing2 Solid Model

2019-12-30
No Thumbnail Available

View/Download File

mAE2_A10000_B - Aircraft.STEP (406.93 MB)

Persistent link to this item

https://hdl.handle.net/11299/214047
Statistics
View Statistics

Journal Title

Journal ISSN

Volume Title

Title

mAEWing2 Solid Model

Authors

Published Date

2019-12-30

Publisher

Type

Dataset

Abstract

mAEWing2 aircraft definition including fabrication, assembly, and testing tooling. The file is a ISO 10303-21 compliant STEP file format. The aircraft centerbody and left wing are provided, the right wing is a mirror of the left.

Keywords

Description

Related to

Replaces

License

Collections

Performance Adaptive Aeroelastic Wing

Series/Report Number

Funding information

NASA NRA NNX14AL36A - "Lightweight Adaptive Aeroelastic Wing for Enhanced Performance across the Flight Envelope”

Isbn identifier

Doi identifier

10.2514/6.2017-1391

Previously Published Citation

Regan, C. D. “mAEWing2: Conceptual Design and System Test.” AIAA Atmospheric Flight Mechanics Conference, 2017, No. January, 2017, pp. 1–20.

Other identifiers

Suggested citation

. (2019). mAEWing2 Solid Model. Retrieved from the University Digital Conservancy, 10.2514/6.2017-1391.

Content distributed via the University Digital Conservancy may be subject to additional license and use restrictions applied by the depositor. By using these files, users agree to the Terms of Use. Materials in the UDC may contain content that is disturbing and/or harmful. For more information, please see our statement on harmful content in digital repositories.