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Development of the NTF-117S Semi-Span BalanceA new high-capacity semi-span force and moment balance has recently been developed for use at the National Transonic Facility at the NASA Langley Research Center. This new semi-span balance provides the NTF a new measurement capability that will support testing of semi-span test models at transonic high-lift testing regimes. Future testing utilizing this new balance capability will include active circulation control and propulsion simulation testing of semi-span transonic wing models. The NTF has recently implemented a new highpressure air delivery station that will provide both high and low mass flow pressure lines that are routed out to the semi-span models via a set high/low pressure bellows that are indirectly linked to the metric end of the NTF-117S balance. A new check-load stand is currently being developed to provide the NTF with an in-house capability that will allow for performing check-loads on the NTF-117S balance in order to determine the pressure tare affects on the overall performance of the balance. An experimental design is being developed that will allow for experimentally assessing the static pressure tare affects on the balance performance.
Document ID
20100019163
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Lynn, Keith C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
May 10, 2010
Subject Category
Aeronautics (General)
Report/Patent Number
NF1676L-10694
NF1676L-10880
Meeting Information
Meeting: 27th AIAA Aerodynamic Measurement and Ground Testing Conference
Location: Chicago, IL
Country: United States
Start Date: June 28, 2010
End Date: July 1, 2010
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 122711.03.09.07.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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