Numerical study of a three-dimensional laminar boundary layer with allowance for coupled heat transfer
Abstract
A solution is presented for the problem of the heating of a spherically blunted cone in the path of a chemically equilibrium or supersonic air flow. The effect of the nonisothermality of the body surface on the characteristics of flow toward the body are analyzed for different angles of attack. Examples of body heating calculations are presented for a wide range of flight velocities. The applicability limits of some traditional approaches are analyzed.
- Publication:
-
PMTF Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki
- Pub Date:
- April 1988
- Bibcode:
- 1988PMTF........34Z
- Keywords:
-
- Aerothermodynamics;
- Boundary Layer Equations;
- Heat Transfer Coefficients;
- Laminar Boundary Layer;
- Supersonic Flow;
- Three Dimensional Boundary Layer;
- Angle Of Attack;
- Nonisothermal Processes;
- Fluid Mechanics and Heat Transfer