TRANSIENT PRESSURE MEASURING METHODS. EFFECTS OF TUBING CONNECTION ON TRANSDUCER RESPONSE

Abstract

Advanced phases of the measurement of transient pressure in rocket chambers is being studied. The measurement of the slower transients, and oscillatory phenome a were i vestigated by means which, although inadequate, represent the common practice in the rocket industry and in most research and development establishments. The validity of such practices as using several inches or more of tubing to connect a transducer into the chamber depends upon the frequency range required, which, of course, is related to the size of the chamber and the mode of instability being examined. Theoretical and experimental treatment of tubing connected transducers was included.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1962
Accession Number
AD0272291

Entities

People

  • Howland B. Jones Jr.

Organizations

  • Princeton University

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeronautical Engineering
  • Combustion
  • Combustion Products
  • Contracts
  • Engineering
  • Frequency
  • Frequency Response
  • Government Procurement
  • Governments
  • Measurement
  • Pressure Measurement
  • Pressure Transducers
  • Resonance
  • Resonant Frequency
  • Shock Tubes
  • Sine Waves
  • Transducers

Readers

  • Control Systems Engineering.
  • Metallurgy
  • Systems Analysis and Design