Abstract
This paper is concerned with an experimental study undertaken to measure the boundary-layer growth on a fan rotor blade. The measurements were carried out at various chordwise and radial locations on both surfaces of the blade using a miniature X configuration hot-wire probe. The streamwise and radial velocity profiles are interpreted and correlated. The validity of conventional velocity profiles, such as the law of the wall for the streamwise profile and the hodograph plot for the cross-flow profile are examined. The measured values of boundary-layer growth properties are compared with the predictions based on a momentum-integral technique. H i
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