20070038956 · Characteristics of Boundary Layer Transition in a Multi-Stage Low-Pressure Turbine
NASA · 2007
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…
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