A CRITICAL REVIEW OF ANALYTICAL METHODS FOR ESTIMATING CONTROL FORCES PRODUCED BY SECONDARY INJECTION: THE TWO DIMENSIONAL PROBLEM,

Abstract

The problem discussed is that of theoretically predicting the normal force induced in the boundary layer separation region immediately ahead of a secondary injection port. Attention was limited to the two-dimensional problem of sonic or supersonic normal injection into supersonic or hypersonic mainstreams. A critical review of available experimental studies was conducted in order to isolate those data best representing a two-dimensional state. The resulting compilation of experimental results was thereafter employed as a basis of comparison for available theoretical and empirical flow models. As a result it was found that analytical means are only capable of rough quantitative estimates of control jet effectiveness and that a more detailed flow model is needed to further explain observed phenomenon. The basic features of such a model are formulated and its conceptual validity demonstrated through comparison with experimental results. Problem areas requiring further research are also discussed in detail. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 04, 1968
Accession Number
AD0669445

Entities

People

  • Michael J. Werle

Organizations

  • Naval Ordnance Laboratory

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Control Jets
  • Layers
  • Secondary Injection
  • Thrust
  • Thrust Control
  • Two Dimensional

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Systems Analysis and Design

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow