Investigation of Rough Running of a Rocket Burner and Observations on "Short Tube" Injection Orifices

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1951
Accession Number
ADA474090

Entities

People

  • F. C. Jessen
  • R. P. Hagerty

Organizations

  • Royal Aircraft Establishment

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Acids
  • Barometric Pressure
  • Coefficients
  • Combustion
  • Diameters
  • Flow Rate
  • Jet Streams
  • Liquid Rocket Propellants
  • Measurement
  • Nitric Acid
  • Physical Properties
  • Reynolds Number
  • Rocket Engines
  • Rocket Propellants
  • Surface Tension
  • Viscosity
  • Water Flow