Accession Number : AD0486376

Title :   EXPERIMENTAL AND DESIGN STUDIES FOR TURBO-RAMJET COMBINATION ENGINE. VOLUME II - CALCULATION ANALYSIS.

Descriptive Note : Final rept.,

Corporate Author : NORD AVIATION CHATILLON-SOUS-BAGNEUX (FRANCE)

Personal Author(s) : Chaulin, P. ; Ravel, M. ; Gozlan, A.

Report Date : JAN 1966

Pagination or Media Count : 138

Abstract : An IBM 7040 computational program, for study of the dimensions, cycle, and performance is described. The calculation procedure for cycle and performance characteristics is detailed. The calculation program for equilibrium composition and for the thermodynamic functions of air and of kerosene-air combustion products is presented.

Descriptors :   (*TURBORAMJET ENGINES, MATHEMATICAL MODELS), COMPUTER PROGRAMMING, THERMODYNAMIC CYCLES, PERFORMANCE(ENGINEERING), CHEMICAL EQUILIBRIUM, THERMAL PROPERTIES, AIR, KEROSENE, TEMPERATURE, ENTROPY, MOLECULAR WEIGHT, ENTHALPY, PRESSURE, SECONDARY FLOW, JET ENGINE INLETS, COMBUSTION, NOZZLE GAS FLOW, TURBOFAN ENGINES, FUEL CONSUMPTION, GAS FLOW, NOZZLE THROATS, VARIABLE AREA NOZZLES, THRUST, MIXTURES, EXHAUST GASES, FRANCE.

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE