Experimental Investigation of Hot-Gas Side Heat-Transfer Rates for a Hydrogen-Oxygen Rocket

Abstract

An experimental investigation was conducted at the Lewis Research center to determine the hot-gas side heat-transfer rates in a rocket nozzle.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1965
Accession Number
ADA393835

Entities

People

  • Ralph L. Schacht
  • Richard J. Quentmeyer
  • William L. Jones

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Combustion
  • Combustion Chambers
  • Enthalpy
  • Equations
  • Gas Turbine Nozzles
  • Heat Sinks
  • Heat Transfer
  • Heat Transfer Coefficients
  • Heat Transmission
  • Hot Gases
  • Instrumentation
  • Liquid Oxygen
  • Materials
  • Measurement
  • Reynolds Number
  • Transport Properties

Readers

  • Combustion and Flow Dynamics.
  • Combustion science or combustion engineering.
  • Fluid Mechanics and Fluid Dynamics.