Transonic Rotor Flow‐Measurement Technique Using Holographic Interferometry
Holographic interferometry is used to record interferograms of the flow near a hovering transonic rotor blade. A pulsed ruby laser recorded 40 interferograms with a 2‐ft‐diam view field near the model rotor‐blade tip operating at a tip Mach number of 0.90. This
paper presents the experimental procedure and example interferograms recorded in the rotor's tip‐path‐plane. In addition, a method currently being pursued to obtain quantitative flow informstion using computer‐assisted tomography (CAT) with the holographic interferogram
data, is outlined.
Document Type: Research Article
Publication date: 01 October 1985
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