TOTAL PRESSURE PROBE FOR A SUPERSONIC GAS FLOW WITH A SLIGHTLY NONUNIFORM VELOCITY FIELD,

Abstract

The object of the invention is a probe of the full pressure in a supersonic flow of a gas with a slightly nonuniform field of velocities representing an axisymmetrical body with pressure-taking tubes. For the purpose of improving the precision of the measure of the full pressure, the contour of the body is designed in the form of an eccentric surface which checks the flow (retarding it) from the supersonic down to the transonic velocity, and the proble tubes are located at the end of the zone of retardation. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 08, 1965
Accession Number
AD0625064

Entities

People

  • M. P. Ryabokon'

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Flow
  • Fluid Flow
  • Gas Flow
  • Intellectual Property
  • Inventions
  • Law
  • Nonuniform
  • Patents
  • Precision
  • Retardation
  • Stratified Fluids
  • Supersonic Flow

Fields of Study

  • Physics

Readers

  • Electrical Engineering
  • Fluid Dynamics.
  • Plasma Physics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow