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Volumn 3991, Issue , 2000, Pages 138-151

Feasibility of using piezoelectric actuators to control launch vehicle acoustics and structural vibrations

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC VARIABLES CONTROL; ACTUATORS; BOUNDARY ELEMENT METHOD; COMPOSITE STRUCTURES; DAMPING; EXTRAPOLATION; LIGHT WEIGHT STRUCTURES; MATHEMATICAL MODELS; PIEZOELECTRIC DEVICES; ROCKETS; STRUCTURAL ANALYSIS; VIBRATION CONTROL;

EID: 0033691389     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (3)

References (27)
  • Reference 정보가 존재하지 않습니다.

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.