Time/frequency analysis of the flutter of the flexible HSCT semispan model

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

Volumn 5, Issue , 2004, Pages 3687-3693

  Chabalko, Christopher C ^a   Hajj, Muhammad R ^a   Silva, Walter A ^b  

^a Virginia Polytechnic Institute and State University   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

Continuous Wavelet Transform; Flutter; Nonlinear aeroelasticity

Indexed keywords

AIR TRANSPORTATION; CIVIL ENGINEERING; DYNAMIC RESPONSE; FOURIER TRANSFORMS; INTEGRAL EQUATIONS; MATHEMATICAL MODELS; OSCILLATIONS; STRAIN GAGES; TRANSDUCERS; WAVELET TRANSFORMS; WIND TUNNELS; WINGS;

CONTINUOUS WAVELET TRANSFORMS; FLEXIBLE SEMISPAN MODEL (FSM); HIGH SPEED CIVIL TRANSPORT (HSCT); NONLINEAR AEROELASTICITY;

FLUTTER (AERODYNAMICS);

EID: 16244375829     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-1856     Document Type: Conference Paper

References (3)

1. W. A. Silva, D. F. Keller, J. R. Florance, S. R. Cole and R. C. Scott, "Experimental Steady and Unsteady Aerodynamic and Flutter Results for HSCT Semispan Models", AIAA/ASME/ASCE/AHS/ASC 41st Structures, Structural Dynamics, and Materials Conference, AIAA 2000-1697, April 2000, Atlanta, GA
2. M. R. Hajj and W. A. Silva, "Nonlinear Flutter Aspects of the Flexible HSCT Semispan Model", Journal of Aircraft, Accepted (2004)
3. P. S. Addison, "The Illustrated Wavelet Transform Handbook: Introductory Theory and Applications in Science, Engineering, Medicine and Finance", Institute of Physics Publishing, 2002