Test Activities in the Langley Transonic Dynamics Tunnel and a Summary of Recent Facility Improvements
Author(s) -
Stanley R. Cole,
Roger K. Johnson,
David J. Piatak,
Jennifer P. Florance,
José A. Rivera
Publication year - 2003
Publication title -
54th aiaa/asme/asce/ahs/asc structures, structural dynamics, and materials conference
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2003-1958
Subject(s) - transonic , aeronautics , aerospace engineering , test (biology) , subsonic and transonic wind tunnel , aerodynamics , environmental science , engineering , computer science , marine engineering , geology , paleontology
The Langley Transonic Dynamics Tunnel (TDT) has provided a unique capability for aeroelastic testing for over 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 compared to testing in air. Higher test medium densities substantially improve model-building requirements and therefore simplify the fabrication process for building aeroelastically scaled wind tunnel models. This paper describes TDT capabilities that make it particularly suited for aeroelasticity testing. The paper also discusses a few recent test activities in the TDT with summaries of several specific tests. Finally, the paper documents recent facility improvement projects and the continuous statistical quality assessment effort for the TDT.
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