An Investigation of Penetration and Spreading for Various Fluids Injected into a Supersonic Stream.

Abstract

A study was conducted to determine the effects of varying the fluid properties of viscosity, surface tension, and density on liquid jet breakup, penetration, and spreading. Water, heptane, and a 58 per cent glycerin-42 per cent water mixture (by mass) were injected transversely into Mach 2.8 and 4.0 airstreams through various circular orifices located in the surface of a flat plate model. Experiments were performed with injector orifices varying in diameter from 0.0145 inches to 0.080 inches, using injectant total pressures ranging from 30 psia. to 3000 psia. Steady-state penetration and lateral spreading distances were measured from scattered light photographs, and qualitative analyses of shock waves induced by the liquid jet were made using schlieren photographs. (Author)

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1968
Accession Number
AD0848875

Entities

People

  • Robert Wellington Castle Jr

Organizations

  • Naval Postgraduate School

Tags

DTIC Thesaurus Topics

  • Diameters
  • Flat Plate Models
  • Injectors
  • Liquid Jets
  • Models
  • Photographs
  • Photography
  • Physical Properties
  • Shock
  • Shock Waves
  • Steady State
  • Surface Tension
  • Viscosity
  • Waves

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow