The procedure for investigating the effect of deviation from flush mounting of pressure transducers on the exterior of Tu-144LL in flight is described. Experimental data in the mach-number range 0.58 - 2.0 are presented for distortion of the measured wall-pressure fluctuation spectra of the turbulent boundary layer by recessed and protruding transducers. The results of flight experiments are compared with data of wind tunnel experiments. The distortion of measured turbulent boundary layer wall pressure fluctuations caused by transducer-surface deviation from the surrounding surface as a function of dimensionless parameters is predicted and presented on the basis of dimensional analysis.
Effect of Transducer Flushness on Measured Surface Pressure Fluctuations in Flight
43rd AIAA Aerospace Sciences Meeting and Exhibit ; 2005 ; Reno, NV, United States
2004-10-18
Preprint
Keine Angabe
Englisch
Effect of transducer flushness on measured surface pressure fluctuations in flight
British Library Conference Proceedings | 2005
|Perceptron tackles gap and flushness
Online Contents | 2002
High Flushness Installation of Countersunk Fasteners
SAE Technical Papers | 2016
|Door open overload: margin and flushness approach
Kraftfahrwesen | 1999
|