An Experimental Investigation of a Transverse Jet Ejecting from a Flat Plate into a Subsonic Free Stream

Abstract

An experimental investigation of the surface static pressures on a flat plate due to a jet injecting transversely into a subsonic free stream was conducted. The free stream Mach numbers were 0.1, 0.2, 0.4, and 0.6 and the jet total pressure ranged from 0 to 1200 psig. The results are presented in tabular form with representative examples of the data shown graphically.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1970
Accession Number
AD0871452

Entities

People

  • Troy A. Street

Tags

Communities of Interest

  • Advanced Electronics

DTIC Thesaurus Topics

  • Boundary Layer
  • Dynamic Pressure
  • Engineering
  • Export Controls
  • Flow
  • Flow Rate
  • Free Stream
  • Government (Foreign)
  • Intellectual Property
  • Mach Number
  • Measurement
  • Network Protocols
  • Photonic Metamaterials
  • Plastic Explosives
  • Pressure Distribution
  • Static Pressure
  • Transverse

Fields of Study

  • Physics

Readers

  • Electromagnetic Wave Scattering and Antenna Radiation Engineering
  • Explosive Engineering.
  • Fluid Dynamics.