Stability analysis for UAVs with a variable aspect ratio wing

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

Volumn 5, Issue , 2005, Pages 3039-3048

  Henry, Janisa J ^a,b,c   Blondeau, Julie E ^b   Pines, Darryll J ^c,d  

^a UNIVERSITY OF MARYLAND   (United States)

^b Rotorcraft Center   (United States)

^c AIAA   (United States)

^d Aerospace Engineering Department   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

TEST DATA; WING MORPHING; WING SWEEP;

ASPECT RATIO; FLIGHT DYNAMICS; WINGS;

UNMANNED VEHICLES;

EID: 28944432676     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

1. Bowman, J., Sanders, B., and Weisshaar, T., "Evaluating the Impact of Morphing Technologies on Aircraft Performance," AIAA Paper 2002-1631, April 2002
2. Sanders, B., Eastep, F. E., and Foster, E., "Aerodynamic and Aeroelastic Characteristics of Wings with Conformal Control faces for Morphing Aircraft," Journal of Aircraft, Vol. 40, No. 1, 2003, pp. 94-99.
3. Amprikidis, M., and Cooper J. E., "Development of Smart Spars for Active Aeroelastic Structures," AIAA Paper 2003-1799, April 2003
4. Blondeau, J., Richeson, J., and Pines, D. J., "Design, Development and Testing of a Morphing Aspect Ratio Wing Using an Inflatable Telescopic Spar," AIAA Paper 2003-1718, April 2003
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9. th AIAA/ASME/AHS/ASC Structures, Structural Dynamics and Materials Conference 2004
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