Generation of transient vibrations on aluminum honeycomb sandwich panels subjected to hypervelocity impacts

International Journal of Impact Engineering

Volumn 35, Issue 12, 2008, Pages 1503-1509

  Francesconi, A ^a   Pavarin, D ^a   Bettella, A ^a   Giacomuzzo, C ^a   Faraud, M ^b   Destefanis, R ^b   Lambert, M ^c   Angrilli, F ^a  

^a UNIVERSITY OF PADOVA   (Italy)

^b THALES ALENIA SPACE ITALIA   (Italy)

^c EUROPEAN SPACE AGENCY   (Netherlands)

Author keywords

Honeycomb sandwich panels; Hypervelocity impact (HVI); Micrometeoroids and orbital debris (M OD); Shock response spectrum (SRS); Vibrations

Indexed keywords

ALUMINA; ALUMINUM; BALLISTICS; DEBRIS; INTERACTIVE COMPUTER SYSTEMS; LATTICE VIBRATIONS; LIGHT METALS; PROJECTILES; SANDWICH STRUCTURES; SPACE DEBRIS; STIMULATED RAMAN SCATTERING; STRUCTURAL PANELS; VIBRATION CONTROL;

HONEYCOMB SANDWICH PANELS; HYPERVELOCITY IMPACT (HVI); MICROMETEOROIDS AND ORBITAL DEBRIS (M/OD); SHOCK RESPONSE SPECTRUM (SRS); VIBRATIONS;

HONEYCOMB STRUCTURES;

EID: 56949087066     PISSN: 0734743X     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijimpeng.2008.07.034     Document Type: Article

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