Characteristics of Boundary Layer Transition in a Multi-Stage Low-Pressure Turbine
20070038956 · NASA · 2007
Public domain · NASATechnical Reports
Overview
An experimental investigation of boundary layer transition in a multi-stage turbine has been completed using surface-mounted hot-film sensors. Tests were carried out using the two-stage Low Speed Research Turbine of the Aerodynamics Research Laboratory of GE Aircraft Engines. Blading in this…
- Publisher
- NASA
- Document
- 20070038956
- Year
- 2007
Source & rights
Source: ntrs.nasa.gov. Public-domain U.S. Government work (17 USC §105) — freely reproducible.
Permanent URL — we don’t break links.
Document details
- Doc number
- 20070038956
- Publisher
- NASA
- Year
- 2007
- File size
- 260 KB