Straight Duct Supersonic Diffuser Flow in a Ludwieg Tube with Upstream Diaphragm.

Abstract

The starting process of supersonic flow in a nozzle followed by constant area, straight duct diffusers was studied in a Ludwieg tube equipped with an upstream diaphragm. The time required to establish steady flow from rest at the exit of the supersonic nozzle was determined from shadowgraph pictures of the flow field, and from static pressure measurements. The initial pressure ratios across the diaphragm to start the supersonic flow at the nozzle exit are also reported. They are compared with the minimum pressure ratio required to sustain the flow at the nozzle exit during the first flow cycle of the Ludwieg tube operation.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1976
Accession Number
ADA037674

Entities

People

  • Nesim Abuaf

Organizations

  • Yale University

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Boundary Layer
  • Flow Fields
  • Flow Rate
  • Mach Number
  • Mass Flow
  • Measurement
  • Pressure Gages
  • Pressure Measurement
  • Pressure Transducers
  • Reynolds Number
  • Shock Tubes
  • Shock Waves
  • Static Pressure
  • Supersonic Diffusers
  • Supersonic Flow
  • Two Dimensional
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow