## Laser Velocimeter Systems Analysis Applied to a Flow Survey Above a Stalled Wing |

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1.5 Frequency airfoil angle of attack average velocity calculated CD CD CD CD CM CJ CJ CJ CM CM CD CM CJ CM CM CM CM eg cn CD cn CM cn cn cn cn eg common volume Correlation Fourier transform Correlations and Fourier Crosscorrelations and autocorrelations data-acquisition dropout zone eg CM eg eg Figure 58 flow field free-stream velocity fringe pattern high-speed burst counter Histograms above transducer histograms with Ul kerosene kurtosis laser beams laser velocimeter measured m/sec with UL Mach number mean velocity measured histograms percent photomultiplier pressure at transducer pressure pulse pressure transducers probability density function reference clock respect to transducer Reynolds number shown in figure Simulated histograms skew smoke standard deviation surface trailing edge transducer 9 transducer position transforms of correlations velocity and standard velocity bias velocity interval velocity measurements vortex model vortices XI XI