Vulnerability of composite aircraft components to fragmenting warheads-experimental analysis, material modeling and numerical studies

Proceedings - 20th International Symposium on Ballistics

Volumn , Issue , 2002, Pages 702-710

  Riedel, W ^a   Thoma, K ^a   Kurtz, A ^b   Collins, P ^c   Greaves, L ^d  

^a FRAUNHOFER INSTITUTE FOR HIGH SPEED DYNAMICS   (Germany)

^b WRIGHT PATTERSON AIR FORCE BASE   (United States)

^c Missiles and Countermeasures   (United Kingdom)

^d QINETIQ   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

BALLISTICS; CARBON FIBER REINFORCED PLASTICS; CARBON FIBERS; CHARACTERIZATION; EXPLOSIVES; FIBER REINFORCED MATERIALS; FIBER REINFORCED PLASTICS; FIGHTER AIRCRAFT; FINITE ELEMENT METHOD; STRAIN GAGES;

ADVANCED COMPOSITE MATERIALS; CARBON FIBRE REINFORCED PLASTIC (CFRP); COMPRESSION AFTER IMPACT TESTS; EXPERIMENTAL ANALYSIS; HYDROCODE SIMULATION; MATERIAL CHARACTERISATION; METALLIC COMPONENT; STRENGTH DEGRADATION;

AIRCRAFT MATERIALS;

EID: 56949085222     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. Gerster T., Riedel W., Orthotropic Strength Properties of HEXCEL IM7/8552, EMI report E 4/02, Ernst-Mach-Institut Freiburg, January 2002
2. N. N., AUTODYN, Theory Manual, Century Dynamics Ltd. Horsham, United Kingdom, 2000
3. Riedel, W, Verwundbarkeit von Flugzeugbauteilen aus Faserverbundwerkstoff, EMI Bericht E 87/00, Freiburg, Germany, December 2000
4. Riedel W., Nahme H., Shock Properties of HEXCEL IM7/8552-Experimental Investigations and Material Modelling, EMI-Report E 25/01, Ernst-Mach-Institut Freiburg, June 2001