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Recent National Transonic Facility Test Process Improvements (Invited)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 feed-forward 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.
Document ID
20010023934
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Kilgore, W. A.
(NASA Langley Research Center Hampton, VA United States)
Balakrishna, S.
(Vigyan Research Associates, Inc. Hampton, VA United States)
Bobbitt, C. W., Jr.
(NASA Langley Research Center Hampton, VA United States)
Adcock, J. B.
(Vigyan Research Associates, Inc. Hampton, VA United States)
Date Acquired
August 20, 2013
Publication Date
January 1, 2001
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA Paper 2001-0756
Meeting Information
Meeting: Aerospace Sciences
Location: Reno, NV
Country: United States
Start Date: January 8, 2001
End Date: January 11, 2001
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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