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International Journal of Non-Linear Mechanics

Volumn 37, Issue 4-5, 2002, Pages 967-986

An aeroelastic model for composite rotor blades with straight and swept tips. Part I: Aeroelastic stability in hover

(3) Friedmann, Peretz P a Yuan, Kuo An a,b De Terlizzi, Marino a

a UNIVERSITY OF MICHIGAN (United States)

b BOEING COMPANY (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ANISOTROPY; COMPOSITE STRUCTURES; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; NONLINEAR EQUATIONS; SHEAR STRESS; TURBOMACHINE BLADES;

COMPOSITE ROTOR BLADES; PLY ORIENTATION;

HELICOPTER ROTORS;

EID: 0036604702 PISSN: 00207462 EISSN: None Source Type: Journal
DOI: 10.1016/S0020-7462(01)00109-3 Document Type: Article

Times cited : (23)

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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.