Inertia Testing and Results

2013-08-10
Loading...
Thumbnail Image

Persistent link to this item

Statistics
View Statistics

Journal Title

Journal ISSN

Volume Title

Title

Inertia Testing and Results

Published Date

2013-08-10

Publisher

Type

Report

Abstract

Description

Included is a report describing the moment of inertia testing done on the Body Freedom Flutter (BFF) aircraft. Pitch inertia was found treating the aircraft as a compound pendulum; roll and yaw inertias were found using the bifilar pendulum technique. Included with the report is a summary of the experimentally determined inertia values.

Related to

Replaces

License

Series/Report Number

Funding information

Isbn identifier

Doi identifier

Previously Published Citation

Other identifiers

Suggested citation

Gupta, Abhineet. (2013). Inertia Testing and Results. Retrieved from the University Digital Conservancy, https://hdl.handle.net/11299/167676.

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.