Integrating CFD and Experiment in Aerodynamics - CFD4Aircraft

Integrating CFD and Experiment in Aerodynamics - CFD4Aircraft Integrating CFD and Experiment in Aerodynamics - CFD4Aircraft

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13.11.2014 Views

Oscillating model α 0 U ∞ Optical head t u v Measuring volume n y min = 0,2 mm Optical fibres Beamexpander turntable y max = 145 mm 45deg mirror Figure 2: ELDV measurements linked with the oscillating frame model

000000000 MEASUREM ENT S MEASUREM ENTS CH 1 CH 2 465 B OSCIL LOSCOP VOLT E S:DIV VOLT S:DIV SETU P SETU P A and B TIME/D IV and D EL AY TIM E SETT INGS BSA enhan ced SETT ING S BSA enhan ced TRIGGER POW ER A TR IGGER SHIFT ENTER SHIFT ENTER Laser source 000000000 Transmitin g block Optical head U V positio nsensor PM1 Optical fibers PM2 Oscillosco p 1 3.95 3.00 4.00 64 10.67 7 8 9 4 5 6 1 2 3 0 . +/- Color separator DANTEC 9.318 1.00 1560 8 0 1 3.9 5 3.00 4.00 10.6 7 64 7 8 9 4 5 6 1 2 3 0 . +/- Postprocessing: Macintos hLabview IEE E DANTE C 9.31 8 1.0 0 1560 8 0 BSA (Burst Spectrum Analyser) Figure 3: ELDV Acquisition chain

Oscillat<strong>in</strong>g model<br />

α 0<br />

U ∞<br />

Optical<br />

head<br />

t<br />

u<br />

v<br />

Measur<strong>in</strong>g<br />

volume<br />

n<br />

y m<strong>in</strong> = 0,2 mm<br />

Optical<br />

fibres<br />

Beamexp<strong>and</strong>er<br />

turntable<br />

y max = 145 mm<br />

45deg mirror<br />

Figure 2: ELDV measurements l<strong>in</strong>ked with the oscillat<strong>in</strong>g frame model

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