Publication Date:
2019-07-13
Description:
This paper describes the results of two recent process improvements; drag feed-forward Mach number control and simultaneous force/moment and pressure testing, at the National Transonic Facility. These improvements have reduced the duration and cost of testing. The drag feedforward Mach number control reduces the Mach number settling time by using measured model drag in the Mach number control algorithm. Simultaneous force/moment and pressure testing allows simultaneous collection of force/moment and pressure data without sacrificing data quality thereby reducing the overall testing time. Both improvements can be implemented at any wind tunnel. Additionally the NTF is working to develop and implement continuous pitch as a testing option as an additional method to reduce costs and maintain data quality.
Keywords:
Research and Support Facilities (Air)
Type:
AIAA Paper 2001-0756
,
Aerospace Sciences; Jan 08, 2001 - Jan 11, 2001; Reno, NV; United States
Format:
application/pdf
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