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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

PARAMETRIC TRENDS & OPTIMIZATION. PRELIMINARY SELECTION OF CONFIGURATION. PROTOTYPE DESIGN & MANUFACTURE = TENDANCES PARAMETRIQUES ET OPTIMISATION. CHOIX PRELIMINAIRE D'UNE CONFIGURATION. CONCEPTION ET FABRICATION DU PROTOTYPEHUBER H.1973; AGARD-LS-63; FR.; DA. 1973; PP. 8.1-8.55; BIBL. 3 P. 1/2; (HELICOPTER AERODYN. DYN.; BRUSSELS; 1973)Conference Proceedings

OPTIMUM PERFORMANCE OF STATIC PROPELLERS AND ROTORS = PERFORMANCE OPTIMALE DES HELICES STATIQUES ET DES ROTORSWU JC; SIGMAN RK; GOORJIAN PM et al.1972; IN: DEV. THEOR. APPL. MECH. PROC. 6TH SOUTHEAST. CONF. TAMPA, FLA, 1972; TAMPA, FLA; 6TH SOUTHEAST. CONF. THEOR. APPL. MECH.; DA. 1972; VOL. 6; PP. 229-252; BIBL. 13 REF.Conference Proceedings

Preference for an inertial degree of freedom describing the teeter motion of windturbine and helicopter rotorsACKVA, J; WEYTH, B.Zeitschrift für angewandte Mathematik und Mechanik. 1991, Vol 71, Num 4, pp T200-T202, issn 0044-2267Article

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

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

Mathematical modelling of a helicopter rotor track and balance : ResultsBEN-ARI, R; ROSEN, A.Journal of sound and vibration. 1997, Vol 200, Num 5, pp 605-620, issn 0022-460XArticle

MEASUREMENT AND ANALYSIS OF ROTOR/PROPELLER NOISEIVES TR; LEVERTON JW.sdIN: CONF. REC. INTERPRETATION ENG. MEAS. PROC.; LONDON; 1972; LONDON; INST. MAR. ENG.; DA. S.D.; PP. 233-248 (9 P.); BIBL. 5 REF.Conference Proceedings

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

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

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

FLAP-LAG STABILITY OF HELICOPTER ROTOR BLADES IN FORWARD FLIGHT.PETERS DA.1975; J. AMER. HELICOPTER SOC.; U.S.A.; DA. 1975; VOL. 20; NO 4; PP. 2-13; BIBL. 10 REF.Article

FIABILITE DES TRANSMISSIONS D'HELICOPTERESLIBEER JP.1973; AERONAUT. ET ASTRONAUT.; FR.; DA. 1973; NO 40; PP. 108-116; ABS. ANGL. ALLEMSerial Issue

2.257.816 (A1) (7500811). - 13 JANVIER 1975. ACCOUPLEMENT SEPARABLE POUR ARBRE D'ENTRAINEMENT.sdPatent

2.280.836 (A1) (75 23964). - 31 JUILLET 1975. TRANSMISSION HARMONIQUE A RAPPORT ELEVE DE REDUCTIONsdPatent

THEORIE TURBULENTE DE L'HELICE DE SUSTENTATIONANIKIN VA.1982; IZV. AKAD. NAUK SSSR, MEH. ZIDK. GAZA; ISSN 0568-5281; SUN; DA. 1982; NO 5; PP. 169-172; BIBL. 7 REF.Article

WIND TUNNEL EVALUATION OF AEROELASTICALLY CONFORMABLE ROTORSBLACKWELL RH; MURRILL RJ; YEAGER WT JR et al.1981; J. AM. HELICOPTER SOC.; ISSN 0002-8711; USA; DA. 1981; VOL. 26; NO 2; PP. 31-39; BIBL. 4 REF.Article

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