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

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

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

AEROSPATIALE PUMA1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 5; PP. 535Serial Issue

THE ROLE OF AERODYNAMICS AND DYNAMICS IN MILITARY AND CIVILIAN APPLICATIONS OF ROTARY WING AIRCRAFT = LE ROLE DE L'AERODYNAMIQUE ET DE LA DYNAMIQUE DANS LES APPLICATIONS MILITAIRES ET CIVILES DES AVIONS A VOILURE TOURNANTEYAGGY PF.1973; AGARD-LS-63; FR.; DA. 1973; PP. 1.1-1.14; (HELICOPTER AERODYN. DYN.; BRUSSELS; 1973)Conference Proceedings

ANALYSIS OF TRANSMISSION FAILURE MODESBOWEN CW.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO 3; PP. 1626-1631; BIBL. 8 REF.Serial Issue

AERODYNAMIC SOURCES OF ROTOR NOISE = SOURCES AERODYNAMIQUES DU BRUIT DES ROTORSCOX CR.1973; J. AMER. HELICOPTER SOC.; U.S.A.; DA. 1973; VOL. 18; NO 1; PP. 3-9; BIBL. 25 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

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

IDENTIFICATION AND OPTIMIZATION OF AIRCRAFT DYNAMICS = IDENTIFICATION ET OPTIMISATION DE LA DYNAMIQUE D'UN AVIONNARENDRA KS; TRIPATHI SS.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 4; PP. 193-199; BIBL. 5 REF.Serial Issue

MILITARY PROGRAMS = PROGRAMMES MILITAIRES1973; SOC. EXPER. TEST PILOTS, TECH. REV.; U.S.A.; DA. 1973; VOL. 11; NO 2; PP. (82 P.); BIBL. 5 REF.Serial Issue

GREASE LUBRICATION OF HELICOPTER TRANSMISSIONS = LUBRIFICATION PAR GRAISSE DES TRANSMISSIONS D'HELICOPTERESCHRISTIAN JB; SIMMONS BR.1973; IN: AM. SOC. LUBR. ENG. 28TH ANNU. MEET. TECH. PREPR.; CHICAGO, ILL.; 1973; PARK RIDGE, ILL.; AMER. SOC. LUBR. ENG.; DA. 1973; PP. 1-10Conference Paper

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

SYMPOSIUM ON HELIPORTS; 19721973; AERONAUT. J.; G.B.; DA. 1973; VOL. 77; NO 749; PP. 217-248; BIBL. DISSEM.Conference Paper

VTOL AIRCRAFTSALKIND MJ.1973; A.S.T.M. SPEC. TECH. PUBL.; U.S.A.; DA. 1973; NO 524; PP. 76-107; BIBL. 17 REF.Serial Issue

INCLUSION OF ROTOR DYNAMICS IN CONTROLLER DESIGN FOR HELICOPTERS = INCLUSION DE LA DYNAMIQUE DU ROTOR DANS LA CONCEPTION D'UN DISPOSITIF DE COMMANDE POUR HELICOPTEREHALL WE JR; BRYSON AE JR.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 4; PP. 200-206; BIBL. 12 REF.Serial Issue

IMPROVING RELIABILITY AND ELIMINATING MAINTENANCE WITH ELASTOMERIC DAMPERS FOR ROTOR SYSTEMSPOTTER JL.1973; J. AMER. HELICOPTER SOC.; U.S.A.; DA. 1973; VOL. 18; NO 1; PP. 23-29; BIBL. 3 REF.Serial Issue

INFLUENCE DU FACTEUR TEMPS SUR L'UTILISATION DES HELICOPTERES POUR LE SERVICE DES PIPE-LINESRASHCHEPKIN KE; STOLYAROV RN.1975; TRANSP. KHRAN. NEFTI NEFTEPROD.; S.S.S.R.; DA. 1975; NO 5; PP. 22-24; BIBL. 4 REF.Article

SOME NOTES ON COLEMAN INSTABILITY.SIMPSON A.1976; AERONAUT. QUART.; G.B.; DA. 1976; VOL. 27; NO 2; PP. 99-111; BIBL. 7 REF.Article

HELICOPTER AVICREW FATIGUEPERRY IC.1974; AGARD-AR-69; FR.; DA. 1974; PP. (25P.); BIBL. 12REF.Report

CONSTRUCTION OF HELIPAD ON MELLUMPLATE LIGHTHOUSE = CONSTRUCTION D'UNE PLATEFORME D'ATTERRISSAGE POUR HELICOPTERE AU PHARE DE MELLUMPLATEMURDEL D.1974; BULL. A.I.S.M.; FR.; DA. 1974; NO 61; PP. 1-4; ABS. FRArticle

AERONAUTICS AND ASTRONAUTICS1972; IN: SUMMER COMPUT. SIMULATION CONF. SAN DIEGO, CALIF., 1972, PROC.; LA JOLLA; SIMULATION COUNC. INC.; DA. 1972; VOL. 1; PP. 641-695; BIBL. DISSEM.Conference Proceedings

ISOLATED AIRFOIL - TIP VORTEX INTERACTION NOISE.PATERSON RW; AMIET RK; MUNCH CL et al.1974; IN: AM. INST. AERONAUT. ASTRONAUT. 12TH AEROSP. SCI. MEET.; WASHINGTON; 1974; NEW YORK; A.I.A.A.; DA. 1974; VOL. 194; PP. 1-9; BIBL. 8 REF.Conference Paper