TASK R

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)

Document Details

Document Type
Technical Report
Publication Date
Dec 31, 1961
Accession Number
AD0271375

Entities

Organizations

  • Johns Hopkins University Applied Physics Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Chemical Kinetics
  • Conductivity
  • Dynamics
  • Energy Transfer
  • Fluid Dynamics
  • Gas Turbine Nozzles
  • Heat Transfer
  • High Temperature
  • Kinetics
  • Measurement
  • Mechanical Equipment
  • Nozzles
  • Rocket Nozzles
  • Rockets
  • Thermal Conductivity

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Fluid Mechanics and Fluid Dynamics.
  • Software Engineering