Body freedom flutter of high aspect ratio flying wings

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

Volumn 3, Issue , 2005, Pages 1808-1830

  Love, Michael H ^a,c   Zink, P Scott ^a,c   Wieselmann, Paul A ^a,c   Youngren, Harold ^b,c  

^a LOCKHEED MARTIN   (United States)

^b Aerocraft Consulting   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLEXIBLE WINGS; FLYING WINGS; FREEDOM FLUTTER; WING STIFFNESS;

APPROXIMATION THEORY; ASPECT RATIO; BENDING (DEFORMATION); FINITE ELEMENT METHOD; FLUTTER (AERODYNAMICS); MATHEMATICAL MODELS;

WINGS;

EID: 28844491807     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

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3. nd International Symposium on Aeroelasticity and Structural Dynamics, Aachen, Germany, April 1985.
4. Jacobson, S.B., Britt, R.T., Dreim, D.R., and Kelly, P.D., "Residual Pitch Oscillation (RPO) Flight Test and Analysis on the B-2 Bomber," AIAA Paper 98-1805
5. Ellis, J., "Body Freedom Flutter Experience on the RB-57F," Presentation given at Aerospace Flutter and Dynamics Council, Spring, 1993.
6. Rodden, W.P., and Johnson, E.H., MSC/NASTRAN Version 68 Aeroelastic Analysis User's Guide, The Macneal-Schwendler Corporation, 1994.
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8. Drela, M., "Integrated Simulation Model for Preliminary Aerodynamic, Structural, and Control-Law Design of Aircraft," AIAA Paper 99-1394.