Accession Number:

AD0271375

Title:

TASK R

Descriptive Note:

Corporate Author:

JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB

Personal Author(s):

Report Date:

1961-12-31

Pagination or Media Count:

1.0

Abstract:

HIGH TEMPERATURE KINETICS IN LAMINAR FLAMES Work continued on the scavenger probe sampling technique for O-atoms in a CH4-O2 flame. THERMAL CONDUCTIVITY OF GASES Tests of the equipment being assembled to furnish known H2O-O2 mixtures for thermal conductivity measurement using the line source technique are described. ROCKET NOZZLE FLUID DYNAMICS Boundary layer pressure and temperature measurements are given for the Mach 4.2 station, and their heat transfer significance discussed. ROCKET NOZZLE CHEMICAL KINETICS A new set of numerical solutions for the flow of a complex propellant gas in the expaning portion of a nozzle are presented. Author

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE