Calculation of the Distribution of Losses over the Span of an Axial-Flow Compressor Blade,
Abstract
On the basis of experimental data, relationships are obtained which make it possible to calculate the losses at each cross section with respect to the height of an axial compressor blade. The obtained results permit a judgment to be made concerning the influence of various cascade parameters upon the distribution of losses with respect to blade height. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 02, 1972
- Accession Number
- AD0750931
Entities
People
- V. S. Beknev
- V. Yu. Kozhevnikov
Organizations
- National Air and Space Intelligence Center