Effects of Nozzle Geometry and Diaphragm Location on the Starting Process in a Ludwieg Tube

Abstract

The starting process in the Ludwieg tube, an intermittent type wind tunnel, was experimentally investigated. Starting flow with varying initial supply gas pressure, nozzle geometry, and downstream diaphragm location, was studied. Two types of closed jet nozzle configurations were used: uniform flow M = 1.6 nozzles, and wedge type M = 1.6 nozzles. Dry air at 1, 2, and 3 atm pressure and room temperature served as the test gas. Starting times were determined from static pressure recordings, made at the exit of the nozzle, and the presence or absence of starting shock waves was confirmed by high speed shadowgraph films of the flow. A dimensional analysis that relates nozzle starting time to the supply conditions, nozzle inlet angle, nozzle contraction ratio, and distance to the diaphragm was performed, and it was found to correlate the measurements.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1973
Accession Number
AD0755357

Entities

People

  • Francis Mosnier
  • Leo T. Smith

Organizations

  • Yale University

Tags

Communities of Interest

  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Cameras
  • Geometry
  • High Speed Cameras
  • Interferometers
  • Light Sources
  • Mach Number
  • Mach Zehnder Interferometers
  • Measurement
  • Munitions
  • Ordnance Laboratories
  • Pressure Measurement
  • Pressure Transducers
  • Static Pressure
  • Steady Flow
  • Wind Tunnels

Readers

  • Combustion science or combustion engineering.
  • Fluid Dynamics.