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Fluctuation measurements in the boundary layer of a supersonic flow

  • Lenz B
  • Gaisbauer U
  • Krämer E
PAMM (2007) 7(1) 4100035-4100036
DOI: 10.1002/pamm.200700729
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Abstract

Fluctuation measurements were carried out via constant‐temperature hot‐wire anemometry inside the turbulent boundary layer of a flat plate and a compression ramp (deflexion angle: 11.5). The free‐stream Mach number was M = 2.54. Fluctuation profiles of the alternating quantities temperature, density and velocity were obtained under the assumption of low pressure fluctuations. (© 2008 WILEY‐VCH Verlag GmbH & Co. KGaA, Weinheim)

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Lenz, B., Gaisbauer, U., & Krämer, E. (2007). Fluctuation measurements in the boundary layer of a supersonic flow. PAMM, 7(1), 4100035–4100036. https://doi.org/10.1002/pamm.200700729

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