Turbine Design System.
Abstract
A time-sharing computer system has been developed which provides for the interactive design and analytical performance evaluation of aircraft engine turbines. The system is modularized to permit the user to deal with one functional aspect of the design at a time; twelve modules are employed to encompass the turbine aerodynamic, heat transfer, and mechanical design. The analytical and numerical methods employed in each module, and their theoretical basis, are presented in this report. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 1978
- Accession Number
- ADA066092
Entities
People
- D. T. Lenahan
- J. S. Keith
- R. D. Caney
- R. R. Wysong
- T. C. Prince
Organizations
- General Electric