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The New Heavy Gas Testing Capability in the NASA Langley Transonic Dynamics TunnelThe NASA Langley Transonic Dynamics Tunnel (TDT) has provided a unique capability for aeroelastic testing for over thirty-five years. The facility has a rich history of significant contributions to the design of many United States commercial transports and military aircraft. The facility has many features which contribute to its uniqueness for aeroelasticity testing; however, perhaps the most important facility capability is the use of a heavy gas test medium to achieve higher test densities. Higher test medium densities substantially improve model building requirements and therefore simplify the fabrication process for building aeroelastically scaled wind-tunnel models. The heavy gas also provides other testing benefits, including reduction in the power requirements to operate the facility during testing. Unfortunately, the use of the original heavy gas has been curtailed due to environmental concerns. A new gas, referred to as R-134a, has been identified as a suitable replacement for the former TDT heavy gas. The TDT is currently undergoing a facility upgrade to allow testing in R-134a heavy gas. This replacement gas will result in an operational test envelope, model scaling advantages, and general testing capabilities similar to those available with the former TDT heavy gas. As such, the TDT is expected to remain a viable facility for aeroelasticity research and aircraft dynamic clearance testing well into the 21st century. This paper describes the anticipated advantages and facility calibration plans for the new heavy gas and briefly reviews several past test programs that exemplify the possible benefits of heavy gas testing.
Document ID
19970015319
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Cole, Stanley R.
(NASA Langley Research Center Hampton, VA United States)
Rivera, Jose A., Jr.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1997
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NAS 1.15:112702
Paper-4
NASA-TM-112702
Report Number: NAS 1.15:112702
Report Number: Paper-4
Report Number: NASA-TM-112702
Meeting Information
Meeting: Royal Aeronautical Society Wind Tunnels and Wind Tunnel Test Techniques Forum
Location: Cambridge
Country: United Kingdom
Start Date: April 14, 1997
End Date: April 16, 1997
Accession Number
97N18261
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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