Gas turbine cycle calculations: Thermodynamic data tables for air and combustion products for three systems of units

Thermodynamic data tabulations specifically designed for gas turbine cycle calculations are presented for 1 ° intervals from 200 K to 2200 K, and from 3500 R to 4000o R. The tables are similar to those of Fielding and Topps, but are rather simpler to use. They are presented in the following systems of units: (a) Engineering Units, K (b)...

Gas turbine cycle calculations thermodynamic data tables for air and combustion products

Thermodynamic data tabulations specifically designed for gas turbine cycle calculations are presented for 1º intervals from 200ºK to 2000ºK, and from 350ºR to 3600°R. The tables are similar to those of Fielding and Topps, but are rather simplier to use, and are available in ºR as well as ºK. Numerical examples illustrating their use are included...

Gas turbine cycle calculations design-point performance of turbojet and turbofan engines

An accurate and comprehensive method for calculating the design-point performance of turbojet and turbofan engines is described in this report . Analyses of the component processes that comprise a cycle are developed in detail from fundamental thermodynamic relations ta the actual equations programmed for the computer. The structure and cading...

Gas turbine cycle calculations: generation of thermodynamic data for dry air and combustion products

A method is presented for generating thermodynamic data (specific heat, enthalpy, and entropy) as functions of temperature and fuel/air ratio, for ranges appropriate to gas turbine cycle calculations. Comparisons of the generally used tabulations of thermodynamic data are made, and specific algebraic expressions are developed which yield results...