The LANN wing is the result of a joint effort between Lockheed, the Air Force, NASA, and the Netherlands to measure unsteady pressures at transonic speeds. It is a moderate-aspect-ratio transport wing configuration. The wing was machined from NITRONIC 40 and has 12 percent thick supercritical airfoil sections.
LANN wing design
1983-03-01
Conference paper
No indication
English
GWLB - Gottfried Wilhelm Leibniz Bibliothek | 2015
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