论文信息 - Fluctuation measurements in the boundary layer of a supersonic flow

Fluctuation measurements in the boundary layer of a supersonic flow

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)

U. Gaisbauer | E. Krämer | B. Lenz

[1] Graham L. Morrison,et al. A study of the constant-temperature hot-wire anemometer , 1971, Journal of Fluid Mechanics.

[2] A. Kistler,et al. Fluctuation Measurements in a Supersonic Turbulent Boundary Layer , 1959 .

[3] L. Kovasznay. Turbulence in Supersonic Flow , 1953 .

[4] L. Kovasznay,et al. The Hot-Wire Anemometer in Supersonic Flow , 1950 .