EFFECT OF THE REYNOLDS NUMBER ON TIP LOSSES,
Abstract
An examination is made of the effect on the Reynolds number on tip losses in foil lattices and under conditions of a rotating turbine stage. The foil lattices were tested on a static stand, while the stages were tested on an experimental turbine. Careful finishing of the blade surfaces excluded the influence of roughness. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 05, 1969
- Accession Number
- AD0700578
Entities
People
- A. S. Maksudyan
- V. A. Chernikov
Organizations
- National Air and Space Intelligence Center