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Related Experiment Video

Updated: Nov 20, 2025

Design and Optimization Strategies of a High-Performance Vented Box
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Optimal Control Surface Layout for an Aeroservoelastic Wingbox.

Bret K Stanford1

  • 1NASA Langley Research Center, Hampton, VA, 23681.

AIAA Journal. American Institute of Aeronautics and Astronautics
|January 22, 2021
PubMed
Summary
This summary is machine-generated.

This study optimizes control surface layouts for aeroservoelastic wingboxes, improving maneuver load alleviation and flutter suppression. The method integrates structural design and actuator placement to minimize mass, revealing key aeroelastic interdependencies.

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Area of Science:

  • Aeroelasticity
  • Aerospace Engineering
  • Computational Mechanics

Background:

  • Aeroservoelasticity combines aerodynamics, structures, and control systems.
  • Maneuver load alleviation and flutter suppression are critical for aircraft safety and performance.
  • Optimizing control surface layout is complex due to coupled aeroelastic effects.

Purpose of the Study:

  • To develop and demonstrate a technique for optimizing the control surface layout of an aeroservoelastic Common Research Model wingbox.
  • To concurrently optimize structural wingbox sizing and control surface actuation variables.
  • To minimize the combined structural and actuator mass while achieving aeroelastic objectives.

Main Methods:

  • Utilized topology optimization principles for combinatorial actuator layout design.
  • Employed layout design variables representing actuator presence (1) or absence (0).
  • Integrated optimization of layout variables with structural sizing and actuation variables.

Main Results:

  • Demonstrated a technique for optimal control surface layout determination.
  • Showcased concurrent optimization of structural and control parameters.
  • Identified significant interdependencies between structural sizing and control surface layout for static and dynamic aeroelastic phenomena.

Conclusions:

  • The proposed technique effectively optimizes control surface layouts for aeroservoelastic applications.
  • Concurrent optimization reveals crucial links between structural design and control strategies.
  • Findings are vital for designing lighter and safer aircraft with enhanced aeroelastic performance.