RESEARCH STUDY TO VERIFY AND EXTEND HIGH SPEED MATH MODEL FOR JET REACTION CONTROL EFFECTIVENESS.

Abstract

An analytical model was developed to predict the performance of a two-dimensional, reaction control jet exhausting normal to supersonic and hypersonic streams. The separation of a turbulent boundary layer upstream of the jet and the pressure field downstream of the jet were studied. A wind tunnel test of a jet slot on a flat plate model was conducted. The existing flow model was revised to give improved accuracy of the predictions of the interference effects upstream of the jet. The flow model was extended to include interference effects downstream of the jet. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1966
Accession Number
AD0645641

Entities

People

  • M. W. Garbrick
  • R. D. Mcdonald

Tags

DTIC Thesaurus Topics

  • Accuracy
  • Boundaries
  • Boundary Layer
  • Control Jets
  • Flat Plate Models
  • Layers
  • Models
  • Turbulent Boundary Layer
  • Two Dimensional
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Combustion and Flow Dynamics.
  • Computational Modeling and Simulation

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow