EXTERNAL BURNING IN SUPERSONIC STREAMS

Abstract

Theoretical and experimental studies of heat addition to external supersonic streams are reviewed, following a brief explanation of the basic fluid mechanical model and possible applications of external burning. Previously developed methods and a new, simplified method for obtaining linearized heat addition solutions are presented. The numerous analyses of combustion via a stationary detonation wave are categorized into four models for planar heat addition, and the equations are developed for the most interesting case of the oblique Chapman-Jouget detonation. The governing equations for a constant-pressure analysis are developed, and performance estimates are given for heat addition adjacent to both double-wedge and flat-plate surfaces. Experimental results of all available external burning tests are discussed, including tests of two-dimensional and axisymmetric bodies. Data are compiled, summarized, and analyzed. The maximum expected pressure coefficient will be near that associated with a separated boundary layer. To obtain the theoretical maximum specific impulse, highly reactive fuels with a combustion length of a few feet will be required.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1967
Accession Number
AD0655460

Entities

People

  • F. S. Billig

Organizations

  • Johns Hopkins University

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Attitude Control Systems
  • Boundary Layer
  • Combustion
  • Combustion Products
  • Combustors
  • Control Surfaces
  • Dynamic Pressure
  • Flow Fields
  • Geometry
  • Models
  • Physics Laboratories
  • Pressure Distribution
  • Pressure Measurement
  • Static Pressure
  • Supersonic Flow
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Fluid Dynamics.
  • Rocket Propulsion.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow