Improvement of the Calculation of Multistaged Turbines of Gas Turbine Engines,
Abstract
The extension of the author's single stage gas turbine improved designing technique (1969) to the calculation of parameters in multistage gas turbine designs is shown. Expressions and nomograms are given for the translation of the previous results to multistage turbine parameter and component analysis and selection. Optimized turbine stage, geometrical characteristics, blade and wheel parameters and multistage gas turbine efficiencies can be determined by using these expressions in computer calculations. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 09, 1971
- Accession Number
- AD0736489
Entities
People
- V. A. Strunkin
Organizations
- National Air and Space Intelligence Center