Plume Observables and Countermeasures

Abstract

Further work on the radiative behavior of rocket exhaust plumes at high altitude is reported. Comparisons of calculated flow fields with wind- tunnel test data indicate that agreement is generally satisfactory if allowances are made for absolute calibrations of the data. Calculations of a plume emission according to some proposed mechanisms have been performed. It appears that production of OH by O atom attack on secondary H atoms in hydrocarbon fragments can result in substantial chemiluminescent emission from H2O formed by subsequent reaction of the OH. Some semi-quantitative analogies between rocket exhaust flows and material releases in the upper atmosphere are discussed, and derivations directed toward comparing collision energy distributions at very high altitudes are presented.

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Document Details

Document Type
Technical Report
Publication Date
Jul 31, 1972
Accession Number
AD0764908

Entities

People

  • Frederick P. Boynton

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Altitude
  • Chemistry
  • Combustion
  • Department Of Defense
  • Exhaust Plumes
  • Flow
  • Flow Fields
  • Fluid Dynamics
  • Gases
  • High Altitude
  • Materials
  • Measurement
  • Physics Laboratories
  • Rocket Exhaust
  • Simulations
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Fluid Dynamics.
  • Molecular Photonics/Laser Physics