File:F-15B 837 Lift and Nozzle Change Effects on Tail Shock (ED09-0008-25).jpg

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Description	English: NASA Dryden's NF-15B tail number 837's canards are tilted down during a pre-flight control check prior to a Lift and Nozzle Change Effects on Tail Shock (LaNCETS) project flight. NASA's Dryden Flight Research Center accomplished a series of flight tests to measure shock waves generated by an F-15 jet in support of the LaNCETS project. The research flights, flown December 2008 through January 2009, provided data to help validate computer models that could be used in designing quieter supersonic aircraft.
Date	Taken on 12 January 2009
Source	https://www.nasa.gov/centers/dryden/multimedia/imagegallery/F-15B_837/ED09-0008-25.html (image link)
Author	NASA/Tony Landis

This image or video was catalogued by Armstrong Flight Research Center of the United States National Aeronautics and Space Administration (NASA) under Photo ID: ED09-0008-25.

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current	05:13, 23 October 2021		3,000 × 2,043 (366 KB)	Huntster (talk \| contribs)	=={{int:filedesc}}== {{Information \|description={{en\|1=NASA Dryden's NF-15B tail number 837's canards are tilted down during a pre-flight control check prior to a Lift and Nozzle Change Effects on Tail Shock (LaNCETS) project flight. NASA's Dryden Flight Research Center accomplished a series of flight tests to measure shock waves generated by an F-15 jet in support of the LaNCETS project. The research flights, flown December 2008 through January 2009, provided data to help validate computer m...

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