Determinate structures for wing camber control
Source abstract
Abstract
An investigation of truss structures for the purpose of creating a continuously variable camber trailing edge device for an aircraft wing is presented. By creating structures that are both statically and kinematically determinate and then substituting truss elements for actuators, it is possible to impose structural deflection without inducing member stress.
Source: openalex_inverted_index · Quality: baseline
Research context
OpenAlex topics: Mechanical Engineering and Vibrations Research · Aerospace Engineering and Control Systems · Vehicle Dynamics and Control Systems
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (25)
Show source-provided references
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