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Volumn 11, Issue 6, 2000, Pages 492-500

Improved helicopter aeromechanical stability analysis using segmented constrained layer damping and hybrid optimization

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; DAMPING; DIMENSIONAL STABILITY; HELICOPTER ROTORS; MATHEMATICAL MODELS; NUMERICAL ANALYSIS; STRUCTURAL ANALYSIS; STRUCTURAL OPTIMIZATION;

EID: 0034197128     PISSN: 1045389X     EISSN: None     Source Type: Journal    
DOI: 10.1106/MH9Y-U9CY-56Q1-L9X4     Document Type: Article
Times cited : (13)

References (11)


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.