Calculation of the thermal regime of a stepped combustion chamber
Abstract
The effective-length method is used to calculate the heat-transfer characteristics and thermal regime of the walls of a stepped scramjet combustor. Based on this method, a formula is proposed for calculating heat transfer between the transition boundary layer and a nonporous surface.
- Publication:
-
TsAGI Uchenye Zapiski
- Pub Date:
- 1985
- Bibcode:
- 1985ZaTsA..16..119B
- Keywords:
-
- Boundary Layer Transition;
- Combustion Chambers;
- Heat Transfer;
- Supersonic Combustion Ramjet Engines;
- Thermal Analysis;
- Wall Temperature;
- Channel Flow;
- Thermal Boundary Layer;
- Fluid Mechanics and Heat Transfer