Development of an adaptive stiffness all-moving vertical tail

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 5, Issue , 2004, Pages 3955-3967

  Amprikidis, Michael ^a   Cooper, Jonathan E ^a   Sensburg, Otto ^b,c  

^a UNIVERSITY OF MANCHESTER   (United Kingdom)

^b AIRBUS GROUP INNOVATIONS   (Germany)

^c School of Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

DEFORMATION; ELASTIC MODULI; FIGHTER AIRCRAFT; FINITE ELEMENT METHOD; FLIGHT DYNAMICS; MATHEMATICAL MODELS; OPTIMIZATION; STIFFNESS; STRUCTURAL DESIGN; TORQUE; WIND TUNNELS;

ACTIVE FLEXIBLE TECHNOLOGY; AEROELASTIC CONSTRAINTS; MULTI-DISCIPLINARY DESIGN OPTIMIZATION (MDO); TORSIONAL STIFFNESS;

EMPENNAGES;

EID: 16244411614     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. th SDM Conference.
2. st SDM Conference, Atlanta.
3. Flick, P. & Love, M. (1999) "The Impact of Active Aeroelastic Wing Technology on Conceptual Aircraft Design'. AVT Panel Meeting. Ottawa.
4. th SDM Conference
5. Pendleton, E.(2000), 'Back to the Future How Active Aeroelastic Wings are a Return to Aviation's Beginnings and a Small Step to Future Bird-like Wings',RTO-SMP Panel Meeting.
6. Schwiger, D. & Krammer, J., (1999) 'Active Aeroelastic Aircraft and its Impact on Stmcture and Flight Control System Design'. AVT Panel Meeting. Ottawa.
7. Wlezien-R-W; Homer-G-C; McGowan-A-R; Padula-S-L; Scott-M -A; Silcox-R-J; Simpson J-O. "The Aircraft Morphing Program" ln:Proc Smart structures and materials meet 1998. pp 176-187
8. Schweiger-J, Suleman A, "The European Research Project - Active Aeroelastic Aircraft Structures" CEAS International Forum on Aeroelasticity and Structural Dynamics, Amsterdam, NL, 2003.