Transonic Thermal Blooming

Abstract

According to the linearized solutions for thermal blooming, the density perturbations become infinite (i.e. 'catastrophic' defocusing) as the Mach number approaches unity. However, the nonlinearities in the transonic equations cutoff the trend to infinity, and the values of the flow perturbation quantities are finite. The nonlinear equations with heat addition are transformed into simple linear algebraic equations through the specification of the streamline geometry in the heat release region. At a Mach number of unity, streamtube area variation was found to be directly proportional to the change in total temperature. A steady, two-dimensional mixed flow solution has been found for the transonic thermal blooming problem. The solution for the density perturbations within a laser beam at a Mach number of precisely unity is given.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1976
Accession Number
ADA026456

Entities

People

  • Edwin F. Carey Jr.

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Atmospheric Attenuation
  • Computational Science
  • Computer Programs
  • Differential Equations
  • Equations
  • Equations Of Motion
  • Fluid Dynamics
  • Fluid Flow
  • Geometry
  • Hydrodynamics
  • Integral Equations
  • Laser Beams
  • Mach Number
  • Refractive Index
  • Thermal Blooming
  • Transonic Flow
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Optical Physics and Photonics.

Technology Areas

  • Directed Energy