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Past, Present, and Future Capabilities of the Transonic Dynamics Tunnel from an Aeroelasticity PerspectiveThe NASA Langley Transonic Dynamics Tunnel (TDT) has provided a unique capability for aeroelastic testing for forty years. The facility has a rich history of significant contributions to the design of many United States commercial transports, military aircraft, launch vehicles, and spacecraft. The facility has many features that contribute to its uniqueness for aeroelasticity testing, perhaps the most important feature being 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. Aeroelastic scaling for the heavy gas results in lower model structural frequencies. Lower model frequencies tend to a make aeroelastic testing safer. This paper will describe major developments in the testing capabilities at the TDT throughout its history, the current status of the facility, and planned additions and improvements to its capabilities in the near future.
Document ID
20000034099
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Cole, Stanley R.
(NASA Langley Research Center Hampton, VA United States)
Garcia, Jerry L.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA Paper 2000-1767
Report Number: AIAA Paper 2000-1767
Meeting Information
Meeting: Dynamics Specialists Conference
Location: Atlanta, GA
Country: United States
Start Date: April 5, 2000
End Date: April 6, 2000
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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