Compressible Turbulent Boundary Layers with Discontinuous Air Transpiration: An Experimental and Theoretical Investigation,
Abstract
Experimental data are presented for the development of compressible turbulent boundary layers moving from a solid onto a transpired surface, and vice versa. The data were obtained at free stream Mach numbers of 1.8 and 3.6 (Reynolds numbers per metre of 2.45 time 10 to the 7th power and 5.45 time 10 to the 7th power respectively) and transpiration rates rho(w)V(w)/rho(1)U(1) up to 0.0044, for nominally zero heat transfer conditions. The resutls are compared with theoretical predictions obtained from a method based on the eddy viscosity concept. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1974
- Accession Number
- ADA041722
Entities
People
- P. G. Marriott