Fig. 6: Bias error assessment.
From: Hypersonic turbulent quantities in support of Morkovin’s hypothesis
Left: Response of the measurement technique to turning on/off different velocity components to assess their effect on \({v}_{\,{{\rm{RMS-Bias}}}\,}^{{\prime} }\). Data labeled with a component includes only those components; e.g., data labeled with \(\overline{u},u{\prime}\) includes only those two components. Right: Response of the measurement technique to variable incident angle θF.
