Accession Number : AD0269927

Title :   CALCULATION PROCEDURE FOR THERMODYNAMIC, TRANSPORT, AND FLOW PROPERTIES OF THE COMBUSTION PRODUCTS OF A HYDROCARBON FUEL MIXTURE BURNED IN AIR WITH RESULTS FOR ETHYLENE-AIR AND METHANE-AIR MIXTURES

Descriptive Note : Technical note

Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON DC

Personal Author(s) : LEYHE, E W ; HOWELL, R R

PDF Url : AD0269927

Report Date : Jan 1962

Pagination or Media Count : 111

Abstract : A procedure is given for de ermining the composition, thermodynamic properties, and transport properties of the dissociated combustion products of a fuel consisting of a mixed hydrocarbon compound burned in air. EQUATIONS AND PROCEDURES FOR DETERMINING SUPERSONIC NOZZLE ORDINATES AND FLOW PROPERTIES FOR THE DISSOCIATED COMBUSTION PRODUCTS ARE PRESENTED. Results are presented for methane and ethylene at the equivalence ratios of 1.0, 0.9, 0.8, a d 0.7 for pressures varying between 1/10,000 and 808 atm and temperatures from 200 to 3,000 K.

Descriptors :   *HYDROCARBONS, *JET ENGINE FUELS, CHEMICAL REACTIONS, COMBUSTION, GAS FLOW, GASES, MATHEMATICAL ANALYSIS, PRESSURE, SUPERSONIC FLOW, TEMPERATURE, THEORY, THERMODYNAMICS, TRANSPORT PROPERTIES

Subject Categories : Organic Chemistry
      Fuels

Distribution Statement : APPROVED FOR PUBLIC RELEASE