A Theoretical Investigation of Axisymmetric Subsonic Diffuser Flow.
Abstract
A marching procedure for solving the finite difference equations describing inviscid, subsonic, compressible flow in an axisymmetric duct is described. The concept of artificial viscosity is introduced and special provisions for maintaining continuity are included. The method predicts the pressure and velocity distributions at any axial station in the duct. A computer program and several sample results are also presented and discussed. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 1973
- Accession Number
- AD0767895
Entities
People
- Kervyn D. Mach
Organizations
- Air Force Research Laboratory