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Aerodynamic Measurements on a Large Splitter Plate for the NASA Langley Transonic Dynamics Tunnel by National Aeronautics and Space Adm Nasa

Aerodynamic Measurements on a Large Splitter Plate for the NASA Langley Transonic Dynamics Tunnel

National Aeronautics and Space Adm Nasa

44 pages missing pub info (editions)

nonfiction science informative medium-paced
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Description

Tests conducted in the NASA Langley Research Center Transonic Dynamics Tunnel (TDT) assess the aerodynamic characteristics of a splitter plate used to test some semispan models in this facility. Aerodynamic data are analyzed to determine the effec...

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