Effects of Elevated Driver-Tube Temperature on the Extent of Quiet Flow in the Purdue Ludwieg Tube.

Abstract

Heated driver-tube air will be needed when the existing Mach-4 test section of the Purdue Quiet-flow Ludwieg tube is replaced with a Mach-6 test section. Thus, a system was developed to heat the air in the driver tube. The air was successfully heated without dramatic adverse effects on the quiet-flow performance. Measurements of the mean and fluctuating pressure were made with a Kulite pressure transducer about 10 cm downstream of the onset of uniform flow. Temperature measurements were made with thermocouples and a cold wire. In agreement with previous results, the cold-driver quiet Reynolds number was about 400,000. The quiet-length Reynolds number decreased with increasing driver-tube temperature, dropping to 380,000 at 90C and 340,000 at 140C. Thus, a nozzle wall that is colder than the gas moves transition forward on the nozzle wall. This trend agrees with Harvey's 1975 observation that a heated nozzle wall delays transition. Problems with nozzle cleanliness were encountered during the heating; there were also problems with maintaining a uniform driver-tube temperature due to heat transfer to the nozzle and to the unheated upstream section of the driver tube.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1996
Accession Number
ADA315654

Entities

People

  • Scott E. Munro

Organizations

  • Purdue University

Tags

Communities of Interest

  • Energy and Power Technologies
  • Sensors
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Boundary Layer Control
  • Computational Fluid Dynamics
  • Fluid Dynamics
  • Fluid Mechanics
  • Heat Transfer
  • Measurement
  • Mechanics
  • Pressure Measurement
  • Pressure Transducers
  • Reynolds Number
  • Swept Wings
  • Temperature Gradients
  • Test And Evaluation
  • Three Dimensional
  • Two Dimensional
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Fluid Dynamics.