Static aeroelastic control for pull-up manuever of a flexible wing with internal actuation

Proceedings of SPIE - The International Society for Optical Engineering

Volumn 4326, Issue , 2001, Pages 307-318

  Khot, N S ^a   Appa, K ^a   Veley, D E ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AERODYNAMIC LOADS; DYNAMIC RESPONSE; ELASTICITY; FORCE CONTROL; ITERATIVE METHODS; LIFT; MANEUVERABILITY; OPTIMAL CONTROL SYSTEMS; SHEAR DEFORMATION; STRAIN; STRUCTURAL DESIGN; SUBSONIC AERODYNAMICS; WINGS;

FLEXIBLE WINGS;

FLEXIBLE STRUCTURES;

EID: 0034768251     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1117/12.436485     Document Type: Conference Paper

References (12)

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3. Executive summary AFTI/F-111 mission adaptive wing
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5. Active flexible wing (AFW) technology
6. An active flexible wing multi - Disciplinary design optimization method
7. Shape memoray alloy adjustable camber (SMAAC) control surfaces
8. Design,fabrication and testing of the DARPA/WL smart wing "wind tunnel model"
9. Smart actuation systems for enhanced aircraft maneuver performance
10. An improved method for the aerodynamic analysis of wing - Body - Tail configurations in subsonic and supersonic flow
11. Automated structural optimization system (ASTROS)