Structural health monitoring of composite plates under ambient and cryogenic conditions

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

Volumn 8, Issue , 2005, Pages 5314-5324

  Engberg, Robert C ^a  

^a NASA MARSHALL SPACE FLIGHT CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CRYOGENIC FUEL TANKS; LAUNCH VEHICLES; SENSOR PLACEMENT STRATEGY; STRUCTURAL HEALTH MONITORING;

ACCIDENT PREVENTION; CATAPULTS (AIRCRAFT LAUNCHERS); CRACKS; CRYOGENIC EQUIPMENT; DELAMINATION; FUEL TANKS; PIEZOELECTRIC DEVICES; SENSORS; STATISTICAL METHODS; STRUCTURAL ANALYSIS; STRUCTURES (BUILT OBJECTS);

COMPOSITE STRUCTURES;

EID: 28844432484     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Engberg, R. and Lassiter, J. Piezoelectric Sensor Impedance Testing Under Vacuum and Cryogenic Conditions. NASA-MSFC test report #NGLT-DEV-03-080, January 2004.
2. Liang, C., Sun. F., and Rodgers, C. Electro-mechanical Impedance Modeling of Active Material Systems. Smart Material Structures, Vol. 5 1996.
3. Peairs, D. Development of a Self-Sensing and Self-Healing Bolted Joint. Master's thesis, Virginia Polytechnic Institute and State University, Blacksburg, VA., July 2002.
4. th ed. New York, NY: McGraw-Hill, 1975.
5. Tseng, K. K. Impedance-based Non-destructive and Non-parametric Infrastructural Performance Evaluation. Journal of Experimental Mechanics. Vol. 44 No.1, Society of Experimental Mechanics, Inc. London, UK: Sage Press, February 2004