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.
ACTE Wing Loads Analysis
Student AIAA meeting ; 2015 ; Columbus, OH, United States
2015-08-04
Miscellaneous
No indication
English
NTIS | 2015
|IuD Bahn | 1998
|AIAA | 1996
|GWLB - Gottfried Wilhelm Leibniz Bibliothek | 1855
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