THE DEFLECTION OF PLANE TURBULENT JETS BY CONVEX WALLS,

Abstract

The effects of geometry and Reynolds number on the attachment of a jet to a convex wall and the mechanism of high pressure recovery in convex-walled amplifiers are investigated. The results are presented in terms of normalized parameters in a form suitable for comparison with theoretical results. Reasonably good agreement is obtained between the experimental results and those predicted theoretically by Gortler and Glauert, particularly for regions of flow away from the control port. The effects of the wall setback and control port are most pronounced in a region near the power nozzle where u sub m/u sub o attains values as high as 1.25. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 27, 1968
Accession Number
AD0673249

Entities

People

  • Turgut Sarpkaya

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Agreements
  • Amplifiers
  • Attachment
  • Deflection
  • Geometry
  • High Pressure
  • Recovery
  • Reynolds Number

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Fluid Mechanics and Fluid Dynamics.