DTIC ADA066092: Turbine Design System pdf

DTIC ADA066092: Turbine Design System

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Description of the Book:

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

• Creator/s: Defense Technical Information Center
• Date: 11/1/1978
• Year: 1978
• Book Topics/Themes: DTIC Archive, Wysong, R R, GENERAL ELECTRIC CO CINCINNATI OHIO AIRCRAFT ENGINE GROUP, *COMPUTER AIDED DESIGN, *GAS TURBINES, HEAT TRANSFER, DATA BASES, STRESS ANALYSIS, MISSION PROFILES, THERMODYNAMICS, MODULAR CONSTRUCTION, SYSTEMS ANALYSIS, GAS TURBINE BLADES, TIME SHARING, AERODYNAMICS, CASCADES(FLUID DYNAMICS

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