Maneuvering Aerothermal Technology (MAT) Program test summary report. Biconic body with slice/flap
Abstract
Detailed shock layer surveys, surface heat transfer and pressure, and force and moment data were obtained on sharp and blunted bicone models tested under laminar and turbulent boundary layer flow conditions. The objective of these tests is to obtain basic body of data under hypersonic flow conditions, and under a variety of flow conditions and geometric parameters which would be useful for checking and validating the newly developed parabolized Navier-Stokes (PNS) codes, and other detailed flow field codes.
- Publication:
-
Final Report
- Pub Date:
- January 1982
- Bibcode:
- 1982sai..reptQ....M
- Keywords:
-
- Aerothermodynamics;
- Conical Bodies;
- Heat Transfer;
- Laminar Boundary Layer;
- Shock Layers;
- Turbulent Boundary Layer;
- Blunt Bodies;
- Hypersonic Flow;
- Navier-Stokes Equation;
- Sharp Leading Edges;
- Fluid Mechanics and Heat Transfer