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Assessment of aerodynamic and dynamic models in a comprehensive analysis for rotorcraftJOHNSON, W.Computers & mathematics with applications. 1986, Vol 12A, Num 1, pp 11-28, issn 0097-4943Article

Rotary-wing aeroelasticity: Current status and future trendsFRIEDMANN, Peretz P.AIAA journal. 2004, Vol 42, Num 10, pp 1953-1972, issn 0001-1452, 20 p.Article

Soft-Histogram Degradation Analysis of a Tie Bar of a Rotor-Head StructureESCAMILLA-AMBROSIO, P. J; LIEVEN, N.Journal of aircraft. 2008, Vol 45, Num 6, pp 2161-2164, issn 0021-8669, 4 p.Article

The role of computerized symbolic manipulation in rotorcraft dynamics analysisCRESPO DA SILVA, M. R. M; HODGES, D. H.Computers & mathematics with applications. 1986, Vol 12A, Num 1, pp 161-172, issn 0097-4943Article

Bruit des hélicoptères = Helicopter noiseLEGENDRE, R.La Recherche aérospatiale. 1984, Num 6, pp 443-445, issn 0034-1223Article

Coupling technique of rotor-fuselage dynamic analysisTANG, D. M; WANG, M. Q.Journal of vibration, acoustics, stress, and reliability in design. 1984, Vol 106, Num 2, pp 235-238, issn 0739-3717Conference Paper

Optimization of Rotorcraft Simultaneous Noninterfering Noise Abatement Approach ProceduresVISSER, H. G; PAVEL, M. D; TANG, S. F et al.Journal of aircraft. 2009, Vol 46, Num 6, pp 2156-2164, issn 0021-8669, 9 p.Conference Paper

Impact damage tolerance of laminated composite helicopter bladesMOROZOV, E. V; SYLANTIEV, S. A; EVSEEV, E. G et al.Composite structures. 2003, Vol 62, Num 3-4, pp 367-371, issn 0263-8223, 5 p.Conference Paper

Smart Spring Control of Vibration on Helicopter Rotor BladesOXLEY, Gregory; NITZSCHE, Fred; FESZTY, Daniel et al.Journal of aircraft. 2009, Vol 46, Num 2, pp 692-696, issn 0021-8669, 5 p.Conference Paper

The future of rotorcraftBYHAM, G. M.Aeronautical Journal. 2003, Vol 107, Num 1072, pp 377-387, issn 0001-9240, 11 p.Article

Vortex cutting by a blade. I: General theory and a simple solutionMARSHALL, J. S.AIAA journal. 1994, Vol 32, Num 6, pp 1145-1150, issn 0001-1452Article

Helicopter rotor noise studies employing advanced testing techniquesHELLER, H.Zeitschrift für angewandte Mathematik und Mechanik. 2001, Vol 81, pp S1037-S1038, issn 0044-2267, SUP4Conference Paper

Helicopter rotor lift distributions for minimum-induced power lossHALL, S. R; YANG, K. Y; HALL, K. C et al.Journal of aircraft. 1994, Vol 31, Num 4, pp 837-845, issn 0021-8669Article

Finite state aeroelastic model for use in rotor design optimizationCHENGJIAN HE; PETERS, D. A.Journal of aircraft. 1993, Vol 30, Num 5, pp 777-784, issn 0021-8669Article

Helicopter rotor dynamics by finite element time approximationBORRI, M.Computers & mathematics with applications. 1986, Vol 12A, Num 1, pp 149-160, issn 0097-4943Article

Aeroelasticity of a Helicopter Blade Using the Euler EquationsGURUSWAMY, Guru P.Journal of aircraft. 2012, Vol 49, Num 2, pp 662-664, issn 0021-8669, 3 p.Article

Effects of reynolds number on characteristics of fixed and rotary wingsSUNADA, S; KAWACHI, K.Journal of aircraft. 2004, Vol 41, Num 1, pp 189-192, issn 0021-8669, 4 p.Article

Computation of transonic flow about helicopter rotor bladesARIELI, R; TAUBER, M. E; SAUNDERS, D. A et al.AIAA journal. 1986, Vol 24, Num 5, pp 722-727, issn 0001-1452Article

Design of helicopter rotor blades for optimum dynamic characteristicsPETERS, D. A; ROSSOW, M. P; KORN, A et al.Computers & mathematics with applications. 1986, Vol 12A, Num 1, pp 85-109, issn 0097-4943Article

Helicopter noise flight tests on the influence of rotor rotational and forward speed changesHELLER, H. H; SPLETTSTOSSER, W. R.Zeitschrift für Flugwissenschaften und Weltraumforschung. 1983, Vol 7, Num 5, pp 322-330, issn 0342-068XArticle

Simulation model for tail rotor failureO'ROURKE, M. J.Journal of aircraft. 1994, Vol 31, Num 1, pp 197-205, issn 0021-8669Article

The use of smooth bending moment modes in helicopter rotor blade vibration studiesDONE, G. T. S; PATEL, M. H.Journal of sound and vibration. 1988, Vol 123, Num 1, pp 71-80, issn 0022-460XArticle

Limit cycle oscillations of a nonlinear rotorcraft modelTONGUE, B. H.AIAA journal. 1984, Vol 22, Num 7, pp 967-974, issn 0001-1452Article

ANALYSE DE L'INFLUENCE DE LA TURBULENCE ATMOSPHERIQUE SUR LE NIVEAU DES CONTRAINTES VARIABLES DE FLEXION DANS LES PALES DE L'HELICE PORTEUSE D'UN HELICOPTERETURKINA AI.1980; IZV. VYSS. UCEBN. ZAVED., AVIAC. TEH.; ISSN 0579-2975; SUN; DA. 1980; NO 2; PP. 83-86; BIBL. 4 REF.Article

Structural dynamics modeling of rectangular rotor bladesTRUONG, Khiem-Van; HYEONSOO YEO; ORMISTON, Robert A et al.Aerospace science and technology (Imprimé). 2013, Vol 30, Num 1, pp 293-305, issn 1270-9638, 13 p.Article

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