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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

SOME PRELIMINARY RESULTS FROM AN INVESTIGATION OF BLADE-VORTEX INTERACTION.HAM ND.1974; J. AMER. HELICOPTER SOC.; U.S.A.; DA. 1974; VOL. 19; NO 2; PP. 45-48; BIBL. 5 REF.Article

A NEW APPROACH TO HELICOPTER WEIGHT FRACTIONS = UNE NOUVELLE APPROCHE DU PROBLEME DES FRACTIONS DE POIDS POUR LES HELICOPTERESHOFFMANN TL; KAMPSCHAFER AR.1973; SOC. EXPER. TEST PILOTS, TECH. REV.; U.S.A.; DA. 1973; VOL. 11; NO 3; PP. 87-99Serial Issue

EQUATIONS DE LA DEFORMATION D'UNE PALE D'HELICE ET PROPRIETES ORTHOGONALES DE SES VIBRATIONS PROPRESLISS A YU.1972; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1972; NO 4; PP. 56-66; BIBL. 7 REF.Serial Issue

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

A PERTURBATION SOLUTION OF HELICOPTER ROTOR FLAPPING STABILITY = UNE SOLUTION PAR PERTURBATION DU PROBLEME DE LA STABILITE DE BATTEMENT D'UN ROTOR D'HELICOPTEREJOHNSON W.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 5; PP. 257-258; BIBL. 4 REF.Serial Issue

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

INSTANTANEOUS VELOCITY MEASUREMENTS IN THE NEAR WAKE OF A HELICOPTER ROTOR.MARESCA C; FAVIER D; REBONT J et al.1974; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1974; VOL. 12; NO 8; PP. 1165-1167; BIBL. 3 REF.Article

HELICOPTER ROTOR BLADESPINCKNEY RL.1973; A.S.T.M. SPEC. TECH. PUBL.; U.S.A.; DA. 1973; NO 524; PP. 108-133; BIBL. 7 REF.Serial Issue

INFLUENCE OF AIRFOILS ON STALL FLUTTER BOUNDARIES OF ARTICULATED HELICOPTER ROTORS = INFLUENCE DES PROFILS SUR LES LIMITES DE FLOTTEMENT DE DECROCHAGE DE ROTORS ARTICULES D'HELICOPTERESBENSON RG; DADONE LU; GORMONT RE et al.1973; J. AMER. HELICOPTER SOC.; U.S.A.; DA. 1973; VOL. 18; NO 1; PP. 36-46; BIBL. 1 REF.Serial Issue

VORTEX NOISE OF ISOLATED AIRFOILS = BRUIT D'ORIGINE TOURBILLONNAIRE DE PROFILS ISOLESPATERSON RW; VOGT PG; FINK MR et al.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 5; PP. 296-302; BIBL. 15 REF.Serial Issue

AERODYNAMIC THEORY FOR WING WITH SIDE EDGE PASSING SUBSONICALLY THROUGH A GUSTMARTINEZ R; WIDNALL SE.1983; AIAA JOURNAL; ISSN 0001-1452; USA; DA. 1983; VOL. 21; NO 6; PP. 808-815; BIBL. 15 REF.Article

STABILITY AND CONTROL OF HINGELESS ROTOR HELICOPTER GROUND RESONANCE.YOUNG MI; BAILEY DJ.1974; J. AIRCR.; U.S.A.; DA. 1974; VOL. 11; NO 6; PP. 333-339; BIBL. 21 REF.Article

MANEUVERABILITY-THEORY AND APPLICATION = THEORIE DE LA MANOEUVRABILITE ET APPLICATIONWELLS CD; WOOD TL.1973; J. AMER. HELICOPTER SOC.; U.S.A.; DA. 1973; VOL. 18; NO 1; PP. 10-22; BIBL. 14 REF.Serial Issue

EFFECT OF PINS WITH FLATS AND RESIN BONDED POLYTETRAFLUORETHYLENE COATINGS ON THE FATIGUE STRENGTH OF LARGE PINNED CONNECTIONS MADE FROM ALLOY STEEL FV520BWHITE DJ.1970; INSTIT. MECH. ENGRS, PROC.; G.B.; DA. 1970; VOL. 185; PART 1; PP. 709-76; BIBL. 11 REF.Serial Issue

VORTEX THEORY FOR HOVERING ROTORSMILLER RH.1982; AIAA J.; ISSN 0001-1452; USA; DA. 1982; VOL. 20; NO 12; PP. 1754-1756; BIBL. 16 REF.Article

COMPLEX COORDINATES IN NEAR HOVERING ROTOR DYNAMICS = COORDONNEES COMPLEXES DANS LA DYNAMIQUE D'UN ROTOR EN VOL QUASI-STATIONNAIRECURTISS HC JR.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 5; PP. 289-296; BIBL. 11 REF.Serial Issue

NOISE GENERATION BY TRANSONIC OPEN ROTORSHAWKINGS DL.1979; MECHANICS OF SOUND GENERATION IN FLOWS. SYMPOSIUM/1979/GOETTINGEN; DEU/USA; BERLIN: SPRINGER-VERLAG/HEIDELBERG: SPRINGER-VERLAG/NEW YORK: SPRINGER-VERLAG; DA. 1979; PP. 294-300; BIBL. 4 REF.Conference Paper

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