A PRELIMINARY STUDY OF THE FLOW FIELD AROUND A BLUNT BODY IN HYPERSONIC LOW DENSITY FLOW.

Abstract

The local temperature and density profiles in the stagnation region of a hemisphere-cylinder body placed in a flow of nitrogen are presented. The Mach number was 9.18, the Reynolds number was 350 per inch and the Knudsen number was 0.045. The stagnation temperature was 298K. The model was cooled with liquid nitrogen. The local density and temperature were measured with an electron beam. The rotational temperature was corrected using Robben and Talbot's experimental curve. The measurements indicate that the local to free stream temperature ratio across the shock layer continuously increases towards the body and reaches a value smaller than the inviscid shock value, whereas the density also increases continuously but reaches a higher value than the inviscid shock value. (Author)

Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1966
Accession Number
AD0645117

Entities

People

  • Duvvuri Tirumalesa

Organizations

  • University of Southern California

Tags

DTIC Thesaurus Topics

  • Blunt Bodies
  • Bodies
  • Electron Beams
  • Flow
  • Flow Fields
  • Free Stream
  • Knudsen Number
  • Low Density
  • Mach Number
  • Nitrogen
  • Reynolds Number
  • Stagnation Temperature

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Mathematics or Statistics
  • Plasma Physics.

Technology Areas

  • Directed Energy
  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow
  • Microelectronics