NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Modifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experimentModifications to the NASA Langley 8 Foot Transonic Pressure Tunnel in support of the Lamina Flow Control (LFC) Experiment included the installation of a honeymoon and five screens in the settling chamber upstream of the test section 41-long test section liner that extended from the upstream end of the test section contraction region, through the best section, and into the diffuser. The honeycomb and screens were installed as permanent additions to the facility, and the liner was a temporary addition to be removed at the conclusion of the LFC Experiment. These modifications are briefly described.
Document ID
19880012663
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Harris, Charles D. (NASA Langley Research Center Hampton, VA, United States)
Brooks, Cuyler W., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1988
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NAS 1.15:4032
NASA-TM-4032
L-16387
Report Number: NAS 1.15:4032
Report Number: NASA-TM-4032
Report Number: L-16387
Accession Number
88N22047
Funding Number(s)
PROJECT: RTOP 505-60-31-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available