Development and verification of an aircraft flutter analysis with uncertainty

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

Volumn 8, Issue , 2007, Pages 7986-7999

  Chung, ChanHoon ^a,c   Shin, SangJoon ^a,c,d   Kim, Taehyoun ^b,e  

^a Seoul National University   (South Korea)

^b BOEING COMPANY   (United States)

^c Seoul National University   (South Korea)

^d AIAA   (United States)

^e Loads and Dynamics ^*

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC FORCES; AERODYNAMIC UNCERTAINTY; AEROELASTIC STABILITY; DOUBLET LATTICE METHOD (DLM);

AIRCRAFT; MACH NUMBER; STABILITY; STIFFNESS; UNCERTAINTY ANALYSIS;

FLUTTER (AERODYNAMICS);

EID: 34547538020     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

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2. Lind, R., "Match-Point Solutions for Robust Flutter Analysis," Journal of Aircraft, Vol. 39, No. 1, 2002, pp.91-99.
3. Borglund, D., "The u-k Method for Robust Flutter Solutions," Journal of Aircraft, Vol. 41, No. 5, 2004, pp. 1209-1216.
4. th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, 2004, pp.1-15.
5. Blair, M.A., A Compilation of the Mathematics Leading to the Doublet Lattice Method, Air Force Wright Laboratory, Dayton, OH, WL-TR-92-3028, March 1992.
6. Hodges, D. H., Introduction to Structural Dynamics and Aeroelasticity, Cambridge University Press, 2002.
7. Goland, M.,"The Flutter of a Uniform Cantilever Wing," Journal of Applied Mechanics, Vol. 12, No. 4, 1945, PP.A197-A208.
8. Zhou, K., Essentials of Robust Control, Prentice Hall, 1998.
9. Lind, R., and Brenner, M., Robust Aeroservoelastic Stability Analysis, Springer, 1999.
10. Karpel, M., "Design for the Active Flutter Suppression and Gust Alleviation Using State-Space Aeroelastic Modeling," Journal of Aircraft, Vol. 19, March 1982, pp. 221-227.