7 x 10 Foot Wind Tunnel

Metadata Updated: March 8, 2017

This wind tunnel is used for basic and applied research in aeromechanics on advanced and unique technology rotorcraft. It supports research on advanced concepts and on problem-solving for current rotorcraft. The test section of this wind tunnel has a maximum speed capability of 100 knots.

Access & Use Information

Public: This dataset is intended for public access and use. License: No license information was provided. If this work was prepared by an officer or employee of the United States government as part of that person's official duties it is considered a U.S. Government Work.

Downloads & Resources

Dates

Metadata Created Date March 8, 2017
Metadata Updated Date March 8, 2017

Metadata Source

Harvested from Federal Laboratory Consortium Data.json

Additional Metadata

Resource Type Dataset
Metadata Created Date March 8, 2017
Metadata Updated Date March 8, 2017
Publisher Federal Laboratory Consortium
Unique Identifier B9F19ABD-515E-4F5C-BDE8-4AEDDDAB4C1B
Maintainer
Maintainer Email
None
Public Access Level public
Address1
Address2
Address3
Metadata Context https://project-open-data.cio.gov/v1.1/schema/catalog.jsonld
Schema Version https://project-open-data.cio.gov/v1.1/schema
Catalog Describedby https://project-open-data.cio.gov/v1.1/schema/catalog.json
Expertise
Fax
Flcbusinessurl https://flcbusiness.federallabs.org/#/laboratory/5443
Harvest Object Id 59c55342-d4e3-4be7-9958-9ae784777ec4
Harvest Source Id 5859cfed-553c-48de-a478-b67b5225f6fc
Harvest Source Title Federal Laboratory Consortium Data.json
Mission
Owneroperatorcode
Phone
Postalcode
Repphone
Sizesqft 0
Source Datajson Identifier True
Source Hash d4f3e5236dc407ca5e09ad2577719a61e5c10916
Source Schema Version 1.1
Statecode CA
T2Website

Didn't find what you're looking for? Suggest a dataset here.