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
01.03.1983
Aufsatz (Konferenz)
Keine Angabe
Englisch
GWLB - Gottfried Wilhelm Leibniz Bibliothek | 2015
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