Accession Number:

AD0384924

Title:

ELEMENT DESIGN AND DEVELOPMENT OF SMALL CENTRIFUGAL COMPRESSOR. VOLUME 2

Descriptive Note:

Technical rept.

Corporate Author:

BOEING CO SEATTLE WA

Personal Author(s):

Report Date:

1967-08-01

Pagination or Media Count:

505.0

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.

Subject Categories:

  • Hydraulic and Pneumatic Equipment

Distribution Statement:

APPROVED FOR PUBLIC RELEASE