Accession Number : AD0690716

Title :   GAS TURBINE CYCLE CALCULATIONS: THERMODYNAMIC DATA TABLES FOR AIR AND COMBUSTION PRODUCTS.

Descriptive Note : Aeronautical rept.,

Corporate Author : NATIONAL AERONAUTICAL ESTABLISHMENT OTTAWA (ONTARIO)

Personal Author(s) : Chappell,M. S. ; Cockshutt,E. P.

Report Date : JAN 1969

Pagination or Media Count : 117

Abstract : Thermodynamic data tabulations specifically designed for gas turbine cycle calculations are presented for 1 deg intervals from 200K to 2000K, and from 350R to 3600R. The tables are similar to those of Fielding and Topps, but are rather simpler to use, and are available in R deg as well as K deg. Numerical examples illustrating their use are included. The polynomial coefficients used to generate the tabular data are also given, should the user wish to evaluate the properties within a computer program. (Author)

Descriptors :   (*GAS TURBINES, *THERMODYNAMICS), AIR, COMBUSTION PRODUCTS, TABLES(DATA), CANADA

Subject Categories : Thermodynamics
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE