Accession Number:

AD0736489

Title:

Improvement of the Calculation of Multistaged Turbines of Gas Turbine Engines,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1971-11-09

Pagination or Media Count:

13.0

Abstract:

The extension of the authors 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

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE