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6x19-Inch Transonic Tunnel

(1972-L-01267): The 6- by 19-inch test section located within the test chamber. Note the test section slots, the airfoil mounted near the top of the test section, and the multiple tubes connecting ports on the airfoil with pressure transducers. Airflow was upward. This is the 6-inch side.

 

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Credit: NASA

Image Number: 1972-L-01267

Date: February 16, 1972

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Uploaded on August 5, 2013
Taken on February 16, 1972