The Effect of Boundary Conditions on the Motion of a Circumferentially Nonuniform Flow in the Axisymmetrical Input Channel of a Compressor,
Abstract
The report examines the effect on the spreading of a circumferentially nonuniform flow of boundary conditions behind the stage and the magnitudes of the axial flow clearance between the input guide device and the drive wheel. In this case the amplitude of the initial nonuniformity of the flow is not assumed to be low.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 04, 1974
- Accession Number
- ADA000158
Entities
People
- L. A. Suslennikov
- S. I. Ginsburg
Organizations
- National Air and Space Intelligence Center