Free-Stream Turbulence Intensity in the Langley 14- by 22-Foot Subsonic Tunnel by Dan H. Neuhart and Catherine B. McGinley (2004, NASA/TP-2004-213247)

NASA/TP-2004-213247 (August 2004). Printed pp. 7–9: hot-wire probes, mean/fluctuating signal channels, calibration and data analysis; Figure 20: sensitivity to retained bandwidth. Summary and flow-quality survey compare positions and operating conditions.