Mach Number Independent Hot-Wire Anemometry

Abstract

A comprehensive characterization of the thermal response of nanoscale hot-wire probes is performed in both subsonic and supersonic flows. A constant current anemometer was designed for the measurement of the intrinsic thermal inertia of hot-wire probes. In particular, the nanoscale probe is considered with the effect of gold-plating on supporting structure of the targeted sensing element. Gold-plated nanoscale probes present a response time one order of magnitude smaller than conventional cylindrical hot-wire probes. Heat transfer simulations show that the temperature profile is considerably modified by the addition of a conductive metal layer, hence increasing the sensor's frequency response in both subsonic and supersonic flows. The increase of frequency response is finally exemplified by the numerical computation of the power spectral density of a turbulent flow signal without any electric compensation of the hot-wire signal.

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Document Details

Document Type
Technical Report
Publication Date
Feb 23, 2023
Accession Number
AD1204559

Entities

People

  • D. C. Barros
  • F. Brunier-coulin
  • Marcus Hultmark
  • Pierre Dupont

Organizations

  • National Center for Scientific Research
  • Princeton University

Tags

Communities of Interest

  • Advanced Electronics
  • Energy and Power Technologies
  • Sensors

DTIC Thesaurus Topics

  • Air Force Research Laboratories
  • Conductivity
  • Equations
  • Fabrication
  • Fluid Dynamics
  • Fluid Flow
  • Fluid Mechanics
  • Frequency
  • Frequency Response
  • Geometry
  • Heat Transfer
  • Heat Transfer Coefficients
  • Mach Number
  • Measurement
  • Supersonic Flow
  • Temperature Gradients
  • Thermal Conductivity
  • Turbulent Flow
  • Turbulent Mixing

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Nanofabrication and Microfabrication.

Technology Areas

  • Hypersonics