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NASA NTRS · 20150018065

ACTE Wing Loads Analysis

Abstract

The Adaptive Compliant Trailing Edge (ACTE) project modified a Gulfstream III (GIII) aircraft with a new flexible flap that creates a seamless transition between the flap and the wing. As with any new modification, it is crucial to ensure that the aircraft will not become overstressed in flight. To test this, Star CCM a computational fluid dynamics (CFD) software program was used to calculate aerodynamic data for the aircraft at given flight conditions.

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BibTeXRIS

Horn, Nicholas R.. 2015-08-04. ACTE Wing Loads Analysis. https://ntrs.nasa.gov/citations/20150018065

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