PRELIMINARY EXPERIMENTAL RESULTS OF THE REDUCTION OF VISCOUS EFFECTS IN A LOW-DENSITY SUPERSONIC NOZZLE BY WALL CRYOPUMPING

Abstract

A low-density supersonic nozzle was operated with carbon dioxide over a range of supply pressures from 10 to 600 microns and the trasition from a boundary layer-inviscid core flow to a full developed viscous flow was observed. A liquidnitrogen cryogenic pump was used to pump the flow through this nozzle. Sizeable reductions of viscous effects in the nozzle flow were observed when the cryogenic pump was extended to the wall of the nozzle. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1961
Accession Number
AD0264656

Entities

People

  • W. N. Macdermott

Organizations

  • Arnold Engineering Development Complex

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Carbon Dioxide
  • Cryopumping
  • Flow
  • Fluid Flow
  • Layers
  • Low Density
  • Nozzles
  • Pumps
  • Supersonic Nozzles
  • Viscous Flow

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.

Technology Areas

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