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Evaluation of turbulence reduction devices for the langley 8-foot transonic pressure tunnel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | McKinney, M. O. Scheiman, J. |
| Copyright Year | 1981 |
| Description | The device test model consisted of a cooler, turning vanes, and settling chamber (immediately upstream of the contraction) in which various combinations of screens and honeycomb were tested. Conventional hot wires were used to measure the axial and lateral turbulence reduction for the different turbulence reduction devices. The final configuration chosen consisted of a honeycomb followed by five screens. |
| File Size | 1540772 |
| Page Count | 40 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810015579 |
| Archival Resource Key | ark:/13960/t08w87g89 |
| Language | English |
| Publisher Date | 1981-06-01 |
| Access Restriction | Open |
| Subject Keyword | Research And Support Facilities (air) Turbulence Laminar Flow Transonic Wind Tunnels Hot-wire Flowmeters Airfoils Wind Tunnel Apparatus Honeycomb Structures Turbulence Meters Guide Vanes Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |