The Effect of Technological Tolerances on Gas Turbine Parameters,
Abstract
A mathematical model of a turbine stage cell is devised such that for any operational condition, all the basic parameters of the turbine can be determined. Solution to the problem was carried out with the usually employed assumptions of turbomachine theory.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 27, 1974
- Accession Number
- ADA004349
Entities
People
- A. E. Tunakov
- Yu. A. Rzhavin
Organizations
- National Air and Space Intelligence Center