Radiative and total heat fluxes from an air plasma to the flat surface of a solid body in the case of shock wave reflection
Abstract
Shock-tube experiments were carried out to measure radiative and total heat fluxes from an air plasma (behind a reflected shock wave) to a flat surface. Heat fluxes were measured by a film-type resistance calorimeter at incident shock wave velocities of up to 10 km/s. It is shown that radiative heat transfer predominates at incident shock wave velocities exceeding 7 km/s at an initial pressure of 1 mm Hg.
- Publication:
-
Problems of Convective and Radiative-Conductive Heat Transfer
- Pub Date:
- 1980
- Bibcode:
- 1980pcrc.book..185K
- Keywords:
-
- High Temperature Air;
- Plasma Dynamics;
- Radiative Heat Transfer;
- Reflected Waves;
- Shock Wave Interaction;
- Solid Surfaces;
- Calorimeters;
- Flat Surfaces;
- Heat Flux;
- Pressure Effects;
- Propagation Velocity;
- Resistance Thermometers;
- Wave Propagation;
- Plasma Physics