Reynolds stress measurements in a three-dimensional supersonic turbulent boundary layer

W. Konrad, Alexander Smits

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Scopus citations

Abstract

Five components of the Reynolds stress tensor were measured in a three-dimensional supersonic turbulent boundary layer. The hot-wire instrumentation and data acquisition procedure were customized for use in this complex flow. Construction, calibration, and operation of the hot-wires are discussed in detail, and a comprehensive uncertainty analysis is included.

Original languageEnglish (US)
Title of host publicationThermal Anemometry 1993
PublisherPubl by ASME
Pages219-230
Number of pages12
ISBN (Print)0791809757
StatePublished - Jan 1 1993
EventProceedings of the Fluids Engineering Conference - Washington, DC, USA
Duration: Jun 20 1993Jun 24 1993

Publication series

NameAmerican Society of Mechanical Engineers, Fluids Engineering Division (Publication) FED
Volume167

Other

OtherProceedings of the Fluids Engineering Conference
CityWashington, DC, USA
Period6/20/936/24/93

All Science Journal Classification (ASJC) codes

  • Engineering(all)

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  • Cite this

    Konrad, W., & Smits, A. (1993). Reynolds stress measurements in a three-dimensional supersonic turbulent boundary layer. In Thermal Anemometry 1993 (pp. 219-230). (American Society of Mechanical Engineers, Fluids Engineering Division (Publication) FED; Vol. 167). Publ by ASME.