Interrogative testing for nonlinear identification of aeroelastic systems

AIAA Journal

Volumn 46, Issue 11, 2008, Pages 2657-2658

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

^a VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c Department of Engineering Science and Mechanics ^*

^d Aeroelasticity Branch

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTIC SYSTEMS; CIVIL TRANSPORTS; DATA ANALYSIS; FLEXIBLE SEMISPAN MODELS; FLIGHT REGIMES; FLOW REGIMES; NASA LANGLEY RESEARCH CENTERS; NON-LINEAR RESPONSES; NONLINEAR IDENTIFICATIONS; NONLINEAR RESPONSE CHARACTERISTICS; RESPONSE CHARACTERISTICS; SWEEP EXCITATIONS; TESTING METHODS; TRANSONIC REGIMES; TRANSONIC TUNNELS;

FLIGHT DYNAMICS; NASA; NONLINEAR CONTROL SYSTEMS;

DATA FLOW ANALYSIS;

EID: 55749095882     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.40092     Document Type: Conference Paper

References (4)

1. Silva, W. A., Keller, D. F., Florance, J. R., Cole, S. R., and Scott, R. C., "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 Paper 2000-1697, Atlanta, GA, Apr. 2000.
2. Hajj, M. R., and Silva, W. A., "Nonlinear Flutter Aspects of the Flexible High-Speed Civil Transport Semispan Model," Journal of Aircraft, Vol. 41, No. 5, 2004, pp. 1202-1208. doi:10.2514/1.2225
3. Chabalko, C. C., Hajj, M. R., and Silva, W. A., "Flutter of High-Speed Civil Transport Flexible Semispan Model: Time Frequency Analysis," Journal of Aircraft, Vol. 43, No. 3, 2006, pp. 743-748. ~doi:10.2514/1.13661
4. Chabalko, C. C., Ge, Z., Hajj, M. R., and Silva, W. A., "Analysis Tools for the Detection of Intermittent Nonlinear Aeroelastic Phenomena," Journal of Aircraft, Vol. 43, No. 4, 2006, pp. 1082-1088. ~doi:10.2514/17639