Determination of the heat conductivity of hot gases from the temperature boundary layer in the shock tube
Abstract
A theory is developed of the pure temperature boundary layer, as is formed after the reflection of the shock wave at the closed end of a shock tube. Then the interference figure is calculated, which occurs when one observes the temperature boundary layer in the differential interferometer.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- 1982
- Bibcode:
- 1982STIN...8321265S
- Keywords:
-
- Boundary Layers;
- Conductive Heat Transfer;
- High Temperature Gases;
- Shock Waves;
- Temperature Distribution;
- Wave Reflection;
- Flow Velocity;
- Gas Pressure;
- Interferometers;
- Shock Tubes;
- Fluid Mechanics and Heat Transfer