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Flow quality studies of the nasa lewis research center 8- by 6-foot supersonic/9- by 15-foot low speed wind tunnel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Pickett, Mark T. Arrington, E. Allen |
| Copyright Year | 1992 |
| Description | A series of studies were conducted to determine the existing flow quality in the NASA Lewis 8 by 6 Foot Supersonic/9 by 15 Foot Low speed Wind Tunnel. The information gathered from these studies was used to determine the types and designs of flow manipulators which can be installed to improve overall tunnel flow quality and efficiency. Such manipulators include honeycomb flow straighteners, turbulence reduction screens, corner turning vanes, and acoustic treatments. The types of measurements, instrumentation, and results obtained from experiments conducted at several locations throughout the tunnel loop are described. |
| File Size | 17379686 |
| Page Count | 48 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19920019430 |
| Archival Resource Key | ark:/13960/t73v4gw83 |
| Language | English |
| Publisher Date | 1992-07-01 |
| Access Restriction | Open |
| Subject Keyword | Research And Support Facilities (air) Turbulence Flow Measurement Measuring Instruments Flow Distribution Vanes Manipulators Wind Tunnel Apparatus Low Speed Wind Tunnels Honeycomb Structures Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
