Effect of Shock Impingement on Heat Transfer. Part II. Effect of Shear Layer Impingement on Pressure and Heat Transfer Rate Distribution around a Cylinder.
Abstract
Static pressure and the heat transfer rate distributions have been measured on the surface of a cylinder in supersonic flow. The cylinder bow shock was intersected by an extraneous oblique shock, the effect of which was to perturb the flow over the cylinder due to the interaction between the shear layer emanating from the intersection points of the shocks and the cylinder boundary layer. The position of this intersection, in relation to the free stream cylinder stagnation point, is shown to have a critical effect upon the pressure and heat transfer rate in the attachment region. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1974
- Accession Number
- AD0778962
Entities
People
- Jean J. Ginoux
- Richard D. Matthews
Organizations
- von Kármán Institute for Fluid Dynamics