ELEMENT DESIGN AND DEVELOPMENT OF SMALL CENTRIFUGAL COMPRESSOR. VOLUME 2
Abstract
The purpose of this program is to facilitate the radial equilibrium analysis of the fluid flow in radial- and mixed-flow impellers for given design conditions. The radial-equilibrium equation is solved at stations normal to the meridional streamlines of an impeller. The total inlet conditions, exit-flow- angle distribution, recovery distribution, and the impeller geometry are inputs to the program. The design results printed out consist of temperatures, pressures, velocities, and angles determined at equilibrium streamlines for the inlet and downstream normal stations. The equilibrium results are used to compute blade surface velocities, which are also program outputs.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1967
- Accession Number
- AD0384924
Entities
People
- A. D. Welliver
- J. Acurio
Organizations
- Boeing