INTERACTION EFFECTS PRODUCED BY A SONIC JET EXHAUSTING FROM A CURVED TWO-DIMENSIONAL PLATE IN A SUPERSONIC STREAM

Abstract

A wind-tunnel investigation was conducted to determine the effects of a sonic jet blowing perpendicular from a curved two-dimensional plate. These tests were performed in the 9 1/2-inch Supersonic Wind Tunnel of the Gas Dynamics Facility at Machine numbers of 2.48, 3.73, and 4.50. Experimental Data are presented for (a) the interaction forces produced by the exhausting jet and the supersonic main stream and (b) the exhausting jet penetration into the supersonic main stream and (c) the exhausting jet penetration into the supersonic main stream. Data were obtained for various slot locations and supply pressures.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1963
Accession Number
AD0404486

Entities

People

  • C. C. Brindle
  • David W. Moxley Jr.

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Boundary Layer
  • Computational Fluid Dynamics
  • Dynamic Pressure
  • Flow
  • Free Stream
  • Layers
  • Mach Number
  • Model Basins
  • Plastic Explosives
  • Pressure Distribution
  • Pressure Measurement
  • Pressure Transducers
  • Static Pressure
  • Supersonic Wind Tunnels
  • Two Dimensional
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Geochemistry

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow