Use of hot-wire anemometry for turbulence measurements in shock induced flowsA research program is currently being conducted with the aim to investigate the operating environment of future gas turbines. The present paper provides a description of the experimental methods which have been employed in performing turbulence intensity measurements in shock-induced flows. In a discussion of the instrumentation, attention is given to the employed low pressure shock tube, the hot-wire probe, the anemometer, the test facility, the experimental setup, the Kistler pressure transducer, and silicon piezoresistive gages. Aspects of instrumentation calibration are considered along with data corrections, experimental data, and data processing.
Document ID
19860055970
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hartung, L. C. (NASA Langley Research Center Hampton, VA, United States)
Duffy, R. E. (Rensselaer Polytechnic Institute, Troy, NY, United States)
Troller, J. W. (Science Applications, Inc. Wayne, PA, United States)