This presentation describes the interface hinge moments loads collected during the ACTE flights.
Evaluation of the Hinge Moment and Normal Force Aerodynamic Loads from a Seamless Adaptive Compliant Trailing Edge Flap in Flight
SciTech 2016 ; 2016 ; San Diego, CA, United States
2016-01-04
Sonstige
Keine Angabe
Englisch
British Library Conference Proceedings | 2016
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