INJECTION OF PARTICLES THROUGH A JET NOZZLE LATERALLY INTO A SUPERSONIC AIRSTREAM

Abstract

Tests were conducted in the 12-in. supersonic tunnel of the von Karman Gas Dynamics Facility to determine the particle distributions downstream of a nozzle exhausting particle-laden flow laterally into the airstream from the tunnel floor. Data were obtained at Mach 3 for a range of jet pressure ratios and nozzle sizes with the nozzles located at several positions upstream of the sampling rake. Reynolds number ranged from 0.15 to 0.62 X 10 to the sixth power per inch. Selected results are presented.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1964
Accession Number
AD0447862

Entities

People

  • E. E. Hilliard

Organizations

  • Arnold Engineering Development Complex

Tags

DTIC Thesaurus Topics

  • Air Force
  • Blast Tubes
  • Boundary Layer
  • Dynamics
  • Flow
  • Free Stream
  • Gas Dynamics
  • Government Procurement
  • Instrumentation
  • Mach Number
  • Particles
  • Pressure Distribution
  • Reynolds Number
  • Sampling
  • Test Equipment
  • Test Facilities
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow