Flexible composite wing with internal actuation for roll maneuver

Journal of Aircraft

Volumn 39, Issue 4, 2002, Pages 521-527

  Khot, N S ^a   Zweber, J V ^a   Veley, D E ^a   Oz H ^b   Eastep, F E ^c  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b OHIO STATE UNIVERSITY   (United States)

^c University of Dayton   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AERODYNAMICS; EMBEDDED SYSTEMS; MANEUVERABILITY; MATHEMATICAL MODELS; STRAIN;

FLEXIBLE COMPOSITE WINGS;

WINGS;

EID: 0036651007     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2971     Document Type: Article

References (7)

1. Wing twist and camber for the rolling maneuver of a flexible wing without ailerons
2. Optimization of a flexible wing without ailerons for the rolling maneuver
3. Design, fabrication, and testing of the DARPA/WL 'smart wing' wind tunnel model
4. Aeroservoelastic design with distributed actuation for high performance aircraft