Aero-optics experimental techniques
Abstract
This report summarizes results of a study to determine the most appropriate aerodynamic experimental techniques for gathering data in aircraft boundary layer and shear layer turbulent flow, flow fields. It focuses on two primary techniques: hot-wire anemometry and five-hole pressure probes, and develops reduction equations for obtaining the desired aerodynamic parameters from raw data. It also presents comparison of hot-wire data using splitfilm probes and x-film probes collected during an airborne experiment.
- Publication:
-
Final Technical Report Spectron Development Labs
- Pub Date:
- July 1984
- Bibcode:
- 1984sdli.rept.....R
- Keywords:
-
- Aerodynamics;
- Boundary Layers;
- Flow Distribution;
- Hot-Wire Anemometers;
- Pressure Sensors;
- Shear Layers;
- Dynamic Pressure;
- Pressure Measurement;
- Fluid Mechanics and Heat Transfer