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Evaluation of mean and turbulent velocity measurements in subsonic accelerated boundary layers
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Seegmiller, H. L. Sandborn, V. A. |
| Copyright Year | 1976 |
| Description | Exploratory measurements of the mean and turbulent flow in the wall boundary layer of a 15.2- by 10.2-cm channel were obtained as part of an instrumentation development program for measurements in compressible flow. Mean surface and flow field surveys were obtained at channel Mach numbers ranging from 0.2 to 0.9. The mean velocity distributions were obtained with total pressure probes and a laser velocimeter. At a channel Mach number of 0.2, several types of hot-wire probes were used to obtain both velocity fluctuations and Reynolds shear-stress results. |
| File Size | 1952315 |
| Page Count | 46 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770004400 |
| Archival Resource Key | ark:/13960/t47q3s188 |
| Language | English |
| Publisher Date | 1976-11-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Mean Laser Doppler Velocimeters Subsonic Flow Flow Distribution Hot-wire Anemometers Turbulent Boundary Layer Velocity Distribution Velocity Measurement Compressible Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
