Accession Number : AD0841524

Title :   COMPUTATION OF THE HEAT CYCLES OF INTERNAL COMBUSTION TURBINES BY A COMPUTER (VYPOCET TEPELNYCH OBEHU SPALOVACICH TURBIN NA SAMOCINNEM POCITACI),

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Personal Author(s) : Kurz, B.

Report Date : 15 SEP 1967

Pagination or Media Count : 8

Abstract : By the example of a three-shaft gas turbine the advantages are demonstrated of using computers for a more accurate calculation of gas cycles. While conventional methods of calculation disregard or simplify many factors, computers can include them in their programs. In the example, the following quantities are included in the formulas: thermodynamic losses in turbines and compressors expressed in isoentropy efficiency, pressure losses, thermal and mechanical losses, losses of the working medium, and combustion process efficiency. (Author)

Descriptors :   (*GAS TURBINES, THERMODYNAMIC CYCLES), INTERNAL COMBUSTION ENGINES, MATHEMATICAL ANALYSIS, COMPUTERS, COMBUSTION CHAMBERS, PERFORMANCE(ENGINEERING), HEAT TRANSFER, CZECHOSLOVAKIA.

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE