NASA NTRS · 20020041761
The Second Generation High Speed Rotor Head Mounted Instrumentation System
Abstract
NASA Ames Research Center has been investigating the air pressure flow of a rotor blade on a UH-60 Black Hawk helicopter in-flight. This paper will address the changes and improvements due to additional restrictions and requirements for the instrumentation system. The second generation instrumentation system was substantially larger and this allowed greatly improved accessibility to the components for ease of maintenance as well as improved gain and offset adjustment capabilities and better filtering.
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Lewis, John, Reynolds, R. S.. 1997-01-01. The Second Generation High Speed Rotor Head Mounted Instrumentation System. https://ntrs.nasa.gov/citations/20020041761
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