Flow quality measurements for the Langley 8-foot transonic pressure tunnel LFC experimentLaminar flow experiments were performed in an 8-foot transonic pressure tunnel which was modified in order to simulate the conditions of an infinite span yawed wing. A liner in the tunnel provided a flow field around the yawed airfoil. The results were evaluated using hot-wire and fluctuating pressure measurements. Data were obtained for root-mean-square fluctuations, their spectra, and various cross product terms.
Document ID
19890037762
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jones, Gregory S. (NASA Langley Research Center Hampton, VA, United States)
Stainback, P. Calvin (NASA Langley Research Center Hampton, VA, United States)
Harris, Charles D. (NASA Langley Research Center Hampton, VA, United States)
Brooks, Cuyler W., Jr. (NASA Langley Research Center Hampton, VA, United States)
Clukey, Steven J. (NASA Langley Research Center Hampton, VA, United States)