High Response Dew Point Measurement System for a Supersonic Wind Tunnel

摘要

A new high response on-line measurement system has been developed to continuously display and record the air stream dew point in the NASA Lewis 10x10 Supersonic Wind Tunnel. Previous instruments suffered from such problems as very slow response, erratic readings, and high susceptibility to contamination. The system operates over the entire pressure level range of the 10x10 SWT, from less than 2 psia to 45 psia, without the need for a vacuum pump to provide sample flow. The system speeds up tunnel testing, provides large savings in tunnel power costs and provides the dew point input for the data-reduction subroutines which calculate test section conditions.